PDS_VERSION_ID = PDS3 PRODUCT_TYPE = "SPK" RECORD_TYPE = "UNDEFINED" INSTRUMENT_NAME = "RADIO SCIENCE SUBSYSTEM" TARGET_NAME = "MOON" DATA_SET_ID = "LRO-L-RSS-1-TRACKING-V1.0" MISSION_NAME = "LUNAR RECONNAISSANCE ORBITER" INSTRUMENT_HOST_NAME = "LUNAR RECONNAISSANCE ORBITER" OBSERVATION_TYPE = "RADIO SCIENCE" PRODUCER_INSTITUTION_NAME = "NASA/GODDARD SPACE FLIGHT CENTER" PRODUCER_ID = "LRO_LOLA_TEAM" PRODUCT_RELEASE_DATE = 2014-12-15 PRODUCER_FULL_NAME = "DAVID E. SMITH" MISSION_PHASE_NAME = "EXTENDED SCIENCE MISSION" PRODUCT_ID = "LRO_ES_10_201311_GRGM900C_L600" PRODUCT_VERSION_ID = "V1.0" PRODUCT_CREATION_TIME = 2013-11-25T00:00:00 START_TIME = 2013-07-18T14:05:01 STOP_TIME = 2013-08-21T16:50:01 ^SPICE_KERNEL = "LRO_ES_10_201311_GRGM900C_L600.BSP" OBJECT = SPICE_KERNEL INTERCHANGE_FORMAT = BINARY KERNEL_TYPE = EPHEMERIS DESCRIPTION = " SPICE kernel file containing spacecraft and target ephemeris data, providing the position and velocity of the spacecraft as a function of time. This ephemeris data is incorporated into LOLA data products. These SPICE kernel files are based on a revised lunar gravity field solution in spherical harmonics to degree and order 900 with a power law constraint applied when the degree exceeds 600 [LEMOINEETAL2014]. The model, GRGM900C, and the kernel files are developed by GRAIL team members and the LOLA Science team at the Goddard Space Flight Center. For information specific to SPK formats and tools, please visit http://naif.jpl.nasa.gov. " END_OBJECT = SPICE_KERNEL END