urn:nasa:pds:lro_radioscience:spice_kernels:lro_es_53_grgm900c_l600.bsp 1.0 1.17.0.0 Product_SPICE_Kernel 2024-05-22 1.0 Initial PDS4 version 2016-11-30T04:30:00Z 2017-01-04T21:30:00Z Observation Geometry Derived Lunar Reconnaissance Orbiter Mission urn:nasa:pds:context:investigation:mission.lunar_reconnaissance_orbiter data_to_investigation Lunar Reconnaissance Orbiter Host urn:nasa:pds:context:instrument_host:spacecraft.lro is_instrument_host Moon Satellite urn:nasa:pds:context:target:satellite.earth.moon data_to_target V1.0 SECOND EXTENDED SCIENCE MISSION NASA/GODDARD SPACE FLIGHT CENTER lro_es_53_grgm900c_l600.bsp 2017-06-01T00:00:00 0 SPICE 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. SPK Binary