urn:nasa:pds:lro_minirf_bistatic:data_derived:lxt_2023229173302_s2_45n341
1.0
Lunar Reconnaissance Orbiter Mini-RF second Stokes Parameter (S2) data, lxt_2023229173302_s2_45n341
1.19.0.0
Product_Observational
2024-11-24
1.0
Initial PDS4 version
2023-08-17T17:33:02.970Z
2023-08-17T17:43:02.798Z
Lunar Reconnaissance Orbiter
Mission
urn:nasa:pds:context:investigation:mission.lunar_reconnaissance_orbiter
data_to_investigation
Lunar Reconnaissance Orbiter
Host
Lunar Reconnaissance Orbiter Spacecraft
urn:nasa:pds:context:instrument_host:spacecraft.lro
is_instrument_host
Mini-RF LRO
Instrument
Mini-RF is a hybrid dual-polarimetric side-looking synthetic aperture radar (SAR) instrument.
urn:nasa:pds:context:instrument:lro.mrflro
is_instrument
Moon
Satellite
urn:nasa:pds:context:target:satellite.earth.moon
data_to_target
RDR
63656
FIFTH EXTENDED SCIENCE MISSION
1/713986382:62644
1/713986982:51333
Johns Hopkins University Applied Physics Laboratory
0
670.0
400.0
4000000000.0
7146200000.0
true
1600000.0
7147000000.0
7147000000.0
5
X
H
2083333.3333333333
3
713986176:32132
DSS-13
BISTATIC
145.59
400970.502
4.650504421588229
53.913
57.032
23.225
2.68326
8.05147
lxt_2023229173302_s2_45n341_v1
display_settings_to_array
Sample
Left to Right
Line
Top to Bottom
lxt_2023229173302_s2_45n341_v1
cartography_parameters_to_image_object
-23.149925595687908
-17.051364703335064
61.12530600660843
29.138290542916078
Oblique Cylindrical
0.0
0.0
45.195348087581806
-19.276136599747346
0.0
4.373929367826095
75.14066845426416
224.63589826040734
0.665185757371798,-0.23263376215852768,0.7095135241090736
0.7015308007318083,-0.1306919241701603,-0.7005527507484992
0.25569990968769496,0.9637433027838225,0.07626534288281933
Coordinate Pair
100.0
100.0
303.2335042414948
303.2335042414948
-486129.0
682.0
Planetocentric
MOON
1737.4
1737.4
1737.4
Positive East
SPK
arecibo.bsp
Provenance Not Applicable
FK
arecibo.tf
Provenance Not Applicable
IK
arecibo.ti
Provenance Not Applicable
SPK
earthstns_itrf93_050714.bsp
Provenance Not Applicable
FK
earth_topo_050714.tf
Provenance Not Applicable
IK
dss13.ti
Provenance Not Applicable
PCK
moon_pa_de421_1900-2050.bpc
Provenance Not Applicable
PCK
pck00010.tpc
Provenance Not Applicable
FK
moon_080317.tf
Provenance Not Applicable
FK
moon_assoc_me.tf
Provenance Not Applicable
FK
earth_assoc_itrf93.tf
Provenance Not Applicable
SPK
de421.bsp
Provenance Not Applicable
LSK
naif0012.tls
Provenance Not Applicable
FK
lro_frames_2010214_v01.tf
Provenance Not Applicable
FK
lro_sandia.tf
Provenance Not Applicable
PCK
earth_000101_231110_230817.bpc
Provenance Not Applicable
SCLK
current.tsc
Mixed
SPK
LRO_DEF_20230817_00.BSP
Mixed
CK
LRO_DEF_20230817_00.BC
Mixed
urn:nasa:pds:lro_minirf_bistatic:browse:lxt_2023229173302_s2_45n341_browse
data_to_browse
Browse JPEG for this product.
lxt_2023229173302_s2_45n341_v1.img
File containing second Stokes Parameter (S2) data.
lxt_2023229173302_s2_45n341_v1
0
2
Last Index Fastest
The second Stokes parameter (S2); represents the difference
between horizontally polarized intensity and the
vertically polarized intensity.
S2 = H * H_con - V * V_con where H and V are the
horizontal and vertical components of the polarized portion
of the received EM field, H_con is the complex conjugate of H
and V_con is the complex conjugate of V.
IEEE754LSBSingle
Line
116
1
Sample
9748
2
-1.0E32
10183087.0
-30308550.0
Minimum, maximum data values; not counting special constants.