PDS_VERSION_ID               = PDS3
RECORD_TYPE                  = FIXED_LENGTH
RECORD_BYTES                 = 1024
^SPICE_KERNEL                = "NAVSPK_OD382P0.BSP"
MISSION_NAME                 = MESSENGER
SPACECRAFT_NAME              = MESSENGER
DATA_SET_ID                  = "MESS-E/V/H-MLA-3/4-CDR/RDR-DATA-V2.0"
KERNEL_TYPE_ID               = SPK
PRODUCT_ID                   = "NAVSPK_OD382P0.BSP"
PRODUCT_CREATION_TIME        = 2017-02-26T00:00:00
PRODUCER_ID                  = {
                               MESSENGER_MLA_TEAM,
                               JHUAPL
                               }
MISSION_PHASE_NAME           = {
                               "MERCURY ORBIT YEAR 5"
                               }
PRODUCT_VERSION_TYPE         = ACTUAL
PLATFORM_OR_MOUNTING_NAME    = "N/A"
START_TIME                   = 2014-201T19:58:32.000
STOP_TIME                    = 2014-218T19:58:32.000 
SPACECRAFT_CLOCK_START_COUNT = "N/A"
SPACECRAFT_CLOCK_STOP_COUNT  = "N/A"
TARGET_NAME                  = {
                               MERCURY
                               }
INSTRUMENT_NAME              = "N/A"
NAIF_INSTRUMENT_ID           = "N/A"
SOURCE_PRODUCT_ID            = "N/A"
NOTE                         = "For reference only: Not for use in scientific
analysis."
OBJECT                       = SPICE_KERNEL
  INTERCHANGE_FORMAT         = BINARY
  KERNEL_TYPE                = EPHEMERIS
  DESCRIPTION                = "This is a fragment of the navigation team's
  predicted orbit solution that was relevant to the time period over which MLA
  data were used to evaluate the spacecraft position at the given time. This
  orbit solution was not modified by the MLA team. It is provided here for
  reference only. The official, final reconstructed trajectory data archived
  at the NAIF PDS node in the data set MESS-E/V/H-SPICE-6-V1.0 should be used
  for all analysis."
END_OBJECT                   = SPICE_KERNEL
END