DAFETF NAIF DAF ENCODED TRANSFER FILE
'NAIF/DAF'
'2'
'6'
'SPKMERGE                                                    '
BEGIN_ARRAY 1 136078
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END_ARRAY 2 3336
BEGIN_ARRAY 3 788
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END_ARRAY 3 788
BEGIN_ARRAY 4 39
'DE-0403LE-0403                          '
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END_ARRAY 4 39
BEGIN_ARRAY 5 136
'DE-0403LE-0403                          '
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END_ARRAY 5 136
BEGIN_ARRAY 6 68
'DE-0403LE-0403                          '
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END_ARRAY 6 68
BEGIN_ARRAY 7 86
'DE-0403LE-0403                          '
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END_ARRAY 7 86
BEGIN_ARRAY 8 74
'DE-0403LE-0403                          '
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END_ARRAY 8 74
BEGIN_ARRAY 9 30
'DE-0403LE-0403                          '
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END_ARRAY 9 30
BEGIN_ARRAY 10 27
'DE-0403LE-0403                          '
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END_ARRAY 10 27
BEGIN_ARRAY 11 24
'DE-0403LE-0403                          '
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END_ARRAY 11 24
BEGIN_ARRAY 12 24
'DE-0403LE-0403                          '
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END_ARRAY 12 24
BEGIN_ARRAY 13 24
'DE-0403LE-0403                          '
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END_ARRAY 13 24
BEGIN_ARRAY 14 209
'DE-0403LE-0403                          '
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'-1746FC^7'
'2A3^5'
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'1CBC7B1EDE0ADF^5'
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'13A577C082281D^-1'
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'2A3^5'
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'1A1459179DEA37^3'
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'-12C64A0612015^1'
'24C7610903143^-1'
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'1C2EE41BC63FBD^-3'
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'-ABA3245B39A73^-5'
'632A64F60EC3B^-6'
'80C2136CC543F^-7'
'-169E3C^7'
'2A3^5'
'-549D5412C4632^5'
'F15F3576DB8898^4'
'3FF2CA3F91C9A2^4'
'-23A1847238BB18^3'
'-357152B6DBC5A6^2'
'1D7944D9B81D79^1'
'254DC62E23CE16^-1'
'-148075A3B0EE^-1'
'60EAF6099D53F4^-3'
'11BB05DD3FA186^-3'
'-3B8224515C544C^-5'
'-F1B1EA234C304^-6'
'DF164312F8488^-7'
'-24BED57AE41A12^5'
'-229D644985100A^5'
'1BED18A49E9DB6^4'
'43722CC4E72A08^3'
'-21FE822CD5CBBE^2'
'-174DDDD90E9918^1'
'16BF78DE138B5A^0'
'-6C63E26F71BF34^-2'
'-119CC19909ACBE^-2'
'360CA8FBFB3318^-4'
'FA6901155D3328^-5'
'-80C3E062B2A4C8^-6'
'-BFE87D44F645F8^-7'
'-7F89CE2FAF771^4'
'-D22D7FA0874EE^4'
'5FAB91A9FE7308^3'
'19FA3346A68657^3'
'-8AA6DBD741CF6^1'
'-A04232C2053BD^0'
'7D4BC30E7FB1AC^-1'
'-123F99D6854A24^-2'
'-695A344B5C02A^-3'
'1AA0318C1EAB63^-5'
'5BF596CA1619D8^-5'
'-1EA2FF51AF8096^-6'
'-512D0B242751DC^-7'
'-1819EC^7'
'546^5'
'29^2'
'5^1'
END_ARRAY 14 209
BEGIN_ARRAY 15 209
'DE-0403LE-0403                          '
'-17DF798^7'
'-16B354^7'
'18F'
'3'
'1'
'2'
209
'-17EFBC^7'
'2A3^5'
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'-1B0D12D079B97A^3'
'FAF49EE719FEA^2'
'7139111370832C^1'
'-152D21D6BBD6A^1'
'-10CE5CF7D7FCC2^0'
'102C5B5C09A24C^-1'
'2203BC79693CBE^-2'
'-74F1CDC75EE9FC^-4'
'-3F88BCD1E92E8A^-4'
'-13F8DB608957E2^-5'
'6F16F8869EFE9^-6'
'64C1EAC420BB38^-7'
'38FB663D255C74^3'
'-7E24C93529A664^3'
'-371264E2CF7A24^2'
'13B41FC4EDFAE6^2'
'A323B99EF07888^0'
'-12821614DD689B^0'
'-169790A28DF4E4^-1'
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'2C15EF405600D6^-3'
'102DBE81DFAFC7^-5'
'-508E2E32D6F4AC^-5'
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'86A5796C4CBA5^-7'
'232FC32A8C3374^3'
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'-1B1C33831DD76D^-5'
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'-12C102A0098B0B^1'
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'-2AB971A20ACA62^-3'
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'468F34A12E5D^-5'
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'-61B9D60B8D46C^-7'
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'345C225024A244^2'
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'-F15D1D0DCCAB38^-4'
'1E5135731F6FF8^-5'
'1B15922CA06BA8^-5'
'-139FA8F735F84B^-6'
'-2A1E45F770F348^-7'
'-1746FC^7'
'2A3^5'
'345D5C0D2CB4C8^3'
'83502F6E57CBC8^3'
'-2FF2CE100A569E^2'
'-137ED986B75C93^2'
'870E8069309AE^0'
'CA4ADC553441C^-1'
'-C64BF7776010A^-2'
'45E1C77AD52E^-3'
'5C9E423B9FD5C^-4'
'-1222BD3B6E093B^-4'
'EE6770B366359^-6'
'B2E55E81AF7C5^-7'
'-215E63F6569B5C^-7'
'-F8213A83A288E8^3'
'152C665A3032E3^3'
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'-594A2D0C17C92^1'
'-1138F775B2684A^1'
'AC4222CBA93DA8^-1'
'4239F1049A00DC^-2'
'-A4627159EBFDE8^-3'
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'-3607A59F942718^-5'
'-1115D75C45E337^-5'
'192C5D2E2F1459^-6'
'-483634E70E8978^-8'
'-5A7C26F31A2718^3'
'-63D00A793A21D8^1'
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'-C7C7E28DCA661^0'
'-691EE52AC01688^0'
'3024D5C930FEC4^-1'
'2345DAECD7EA8C^-2'
'-3DDCD522E720CC^-3'
'3E0643A88D3B8^-4'
'-1905B143B23291^-6'
'-6E70EFB6795464^-6'
'82C8D902E4BA5^-7'
'6CEA663510F428^-9'
'-16F29C^7'
'2A3^5'
'FD435D81A3703^3'
'3D211F2D45DCC2^3'
'-D184D177B19DF^2'
'-6680F4EC44D944^1'
'F2FAF12B42F788^0'
'-46694F3C15D074^-2'
'-610A99FCEC7104^-2'
'1BF15CA8EE8A04^-3'
'3D6043645F8432^-5'
'41F2B4DA948998^-5'
'-26AB901E178ACA^-6'
'-5B9496434D91E4^-7'
'5A5943B546EFAC^-8'
'-6F3425473EFBAC^3'
'6C52A4833FE454^3'
'5F01975417A368^2'
'-FAD81429B724D^1'
'-316FCE1ABC2B38^0'
'A7819EA570584^-1'
'-25B0D657902688^-2'
'-2037625AF4AA6A^-3'
'-EE03B6A2E9CAB^-5'
'9636893B4D943^-6'
'594028897DEF9C^-6'
'-47345827F1A0C^-7'
'-385DFDB3AE34B4^-8'
'-3638F79075FFD^3'
'228CEA8496D336^3'
'2E2A2A7C1B23DC^2'
'-521E8B28DFC66^1'
'-204F8E2B7DCE82^0'
'3B1E15F2BE0916^-1'
'-73CF3A8AAF2604^-3'
'-D068DC1BEA7D9^-4'
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'21C73F559DB99E^-6'
'-13840E71E404C9^-7'
'-1956F468E4AFFB^-8'
'-169E3C^7'
'2A3^5'
'10A6F61D72888B^4'
'-2F808B43E7FD62^3'
'-C95C7CFC1ECAD8^2'
'7031EA18A5EA1C^1'
'A847DEFA121D58^0'
'-5CCE9C07A6B2AC^-1'
'-757669C427E248^-3'
'408E654D748EAC^-3'
'-1312CF92E58A31^-4'
'-37D483F2265338^-5'
'BB61668330C868^-7'
'2F90D20F21AEAC^-7'
'-2BE754C1EA6D1^-8'
'73B452594649DC^3'
'6CFED41E344104^3'
'-57EF232F652608^2'
'-D45FE2499584C^1'
'6B0A891D620E54^0'
'49615F97F60688^-1'
'-47A1002084B9A4^-2'
'1554CC8A68FB0E^-3'
'37753622D637E^-4'
'-AA30FF5BE89EA^-6'
'-3147E67470073^-6'
'19574F20866184^-7'
'25C48389751EF2^-8'
'19197FEE0B358D^3'
'295CF3A9D25174^3'
'-12D3F44CCB66F4^2'
'-51CC359CA343E4^1'
'1B4968652311CF^0'
'1F89FA7C97346E^-1'
'-18A8871448EDDA^-2'
'3975FA6F532572^-4'
'14BBC0473AEFE5^-4'
'-53D6E3F2E4786^-7'
'-1218FF6A17AE4D^-6'
'6078196ABCFCA4^-8'
'FF9B8889B14608^-9'
'-1819EC^7'
'546^5'
'29^2'
'5^1'
END_ARRAY 15 209
BEGIN_ARRAY 16 12
'DE-0403LE-0403                          '
'-17DF798^7'
'-16B354^7'
'C7'
'1'
'1'
'2'
12
'-32CC4C^7'
'AB63^7'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-DE2F4C^7'
'156C6^8'
'8^1'
'1^1'
END_ARRAY 16 12
BEGIN_ARRAY 17 12
'DE-0403LE-0403                          '
'-17DF798^7'
'-16B354^7'
'12B'
'2'
'1'
'2'
12
'-32CC4C^7'
'AB63^7'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-DE2F4C^7'
'156C6^8'
'8^1'
'1^1'
END_ARRAY 17 12
BEGIN_ARRAY 18 64
'MAR033.2                                '
'-17DF798^7'
'-16B354^7'
'1F3'
'4'
'1'
'3'
64
'-18399^7'
'5EEC^5'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-177BB8^7'
'5EEC^5'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-16BDE^7'
'5EEC^5'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'0^0'
'-18987C^7'
'BDD8^5'
'14^2'
'3^1'
END_ARRAY 18 64
TOTAL_ARRAYS 18
 ~NAIF/SPC BEGIN COMMENTS~
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-07-28/07:31:11.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990318.990324.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; MERGE.SPK.bsp LOG FILE
;
; Created 1999-04-07/05:48:18.00.
;
; SPKMERGE BEGIN COMMANDS

LEAPSECONDS_KERNEL   = /geod8/MGS/kernels/naif0007.tls

SPK_KERNEL           = MERGE.SPK.bsp
  SOURCE_SPK_KERNEL  = SPKNEW.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = -94
    BEGIN_TIME       = 1999 MAR 18 18:01:39.998
    END_TIME         = 1999 MAR 23 23:58:19.998
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 401
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 402
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 4
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 1
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 2
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 3
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 10
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 5
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 6
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 7
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 8
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 9
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 301
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 399
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 199
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 299
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814
  SOURCE_SPK_KERNEL  = /ares4/MGS/spk.files/spk990317.d107.bsp
    INCLUDE_COMMENTS = YES
    BODIES           = 499
    BEGIN_TIME       = 1999 MAR 17 18:28:55.814
    END_TIME         = 1999 MAR 31 23:58:55.814

; SPKMERGE END COMMANDS

PRODUCT NAME = NASA POE
NAIF SPICE Spacecraft ID: -94
NAIF SPICE Center ID: 499
NAIF SPICE Frame: J2000
NAIF SPICE Internal Filename:
        MGS arc 98.${BM}.${BD}.${BT}:00                         !
Lagrange Interpolating Degree: 9
Semi Major Axis: 3.39700E+03 km
Reciprocal flattening: 1.54409E+02
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
; spk_m_990317_OD107-120_281_V1.bsp LOG FILE
;
; Created 1999-03-18/23:07:27.00.
;
; BEGIN NIOSPK COMMANDS

LEAPSECONDS_FILE    = /local/naif/samples/naif0007.tls
SPK_FILE            = spk_m_990317_OD107-120_281_V1.bsp
  SPK_LOG_FILE      = spk_m_990317_OD107-120_281_V1.cmd.log
  INCLUDE_TEXT_FILE = /local/naif/samples/naif0007.tls
  SOURCE_NIO_FILE   = p_m_990317_OD107-120_281_V1.nio
    BODIES          = -94
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/de403_1993-2004.nio
    BODIES          = 1 2 3 4 5 6 7 8 9 10 301 399 199 299 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000
  SOURCE_NIO_FILE   = /local/naif/ephemeris/se_mar033.2_1997-2000.nio
    BODIES          = 401 402 499
    BEGIN_TIME      = CAL-ET 1999 MAR 17 18:30:00.000
    END_TIME        = CAL-ET 1999 APR 01 00:00:00.000

; END NIOSPK COMMANDS

LEAPSECONDS KERNEL FILE
===========================================================================

Modifications:
--------------
1998, Jul  17   WLT  Modified file to account for the leapsecond that
                     will occur on December 31, 1998.

1997, Feb  22   WLT  Modified file to account for the leapsecond that
                     will occur on June 30, 1997.

1995, Dec  14   KSZ  Corrected date of last leapsecond from 1-1-95
                     to 1-1-96.

1995, Oct  25   WLT  Modified file to account for the leapsecond that
                     will occur on Dec 31, 1995.

1994, Jun  16   WLT  Modified file to account for the leapsecond on
                     June 30, 1994.

1993, Feb. 22  CHA   Modified file to account for the leapsecond on
                     June 30, 1993.

1992, Mar. 6   HAN   Modified file to account for the leapsecond on
                     June 30, 1992.

1990, Oct. 8   HAN   Modified file to account for the leapsecond on
                     Dec. 31, 1990.


Explanation:
------------

The contents of this file are used by the routine DELTET to compute the
time difference

[1]       DELTA_ET  =  ET - UTC

the increment to be applied to UTC to give ET.

The difference between UTC and TAI,

[2]       DELTA_AT  =  TAI - UTC

is always an integral number of seconds. The value of DELTA_AT was 10
seconds in January 1972, and increases by one each time a leap second
is declared. Combining [1] and [2] gives

[3]       DELTA_ET  =  ET - (TAI - DELTA_AT)

                    =  (ET - TAI) + DELTA_AT

The difference (ET - TAI) is periodic, and is given by

[4]       ET - TAI  =  DELTA_T_A  + K sin E

where DELTA_T_A and K are constant, and E is the eccentric anomaly of the
heliocentric orbit of the Earth-Moon barycenter. Equation [4], which ignores
small-period fluctuations, is accurate to about 0.000030 seconds.

The eccentric anomaly E is given by

[5]       E = M + EB sin M

where M is the mean anomaly, which in turn is given by

[6]       M = M  +  M t
               0     1

where t is the number of ephemeris seconds past J2000.

Thus, in order to compute DELTA_ET, the following items are necessary.

          DELTA_TA
          K
          EB
          M0
          M1
          DELTA_AT      after each leap second.

The numbers, and the formulation, are taken from the following sources.

     1) Moyer, T.D., Transformation from Proper Time on Earth to
        Coordinate Time in Solar System Barycentric Space-Time Frame
        of Reference, Parts 1 and 2, Celestial Mechanics 23 (1981),
        33-56 and 57-68.

     2) Moyer, T.D., Effects of Conversion to the J2000 Astronomical
        Reference System on Algorithms for Computing Time Differences
        and Clock Rates, JPL IOM 314.5--942, 1 October 1985.

The variable names used above are consistent with those used in the
Astronomical Almanac.

\begindata

DELTET/DELTA_T_A       =   32.184
DELTET/K               =    1.657D-3
DELTET/EB              =    1.671D-2
DELTET/M               = (  6.239996D0   1.99096871D-7 )

DELTET/DELTA_AT        = ( 10,   @1972-JAN-1
                           11,   @1972-JUL-1
                           12,   @1973-JAN-1
                           13,   @1974-JAN-1
                           14,   @1975-JAN-1
                           15,   @1976-JAN-1
                           16,   @1977-JAN-1
                           17,   @1978-JAN-1
                           18,   @1979-JAN-1
                           19,   @1980-JAN-1
                           20,   @1981-JUL-1
                           21,   @1982-JUL-1
                           22,   @1983-JUL-1
                           23,   @1985-JUL-1
                           24,   @1988-JAN-1
                           25,   @1990-JAN-1
                           26,   @1991-JAN-1
                           27,   @1992-JUL-1
                           28,   @1993-JUL-1
                           29,   @1994-JUL-1
                           30,   @1996-JAN-1
                           31,   @1997-JUL-1
                           32,   @1999-JAN-1 )


\beginlabel
MISSION_NAME = MARS_GLOBAL_SURVEYOR
SPACECRAFT_NAME = MARS_GLOBAL_SURVEYOR
DATA_SET_ID = MO-M-SPICE-6-SPK-V1.0
FILE_NAME = spk_m_990317_OD107-120_281_V1
PRODUCT_ID = SPK
PRODUCT_VERSION_TYPE = SPK-V1.0
MISSION_PHASE_TYPE = MAPPING
PRODUCT_CREATION_TIME = 1999-077T23:12:02
START_TIME = 1999-03-17T18:30:00.000
STOP_TIME = 1999-04-01T00:00:00.000
PRODUCER_ID = NAV
NOTE = ''
\endlabel
 ~NAIF/SPC END COMMENTS~