MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "080523BP_SCPSE_08144_08155.xsp" PRODUCT_CREATION_TIME = 2008-05-23T13:12:28 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-05-22T13:56:55 STOP_TIME = 2008-06-03T11:58:55 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "CASSINI", "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS", "MIMAS", "ENCELADUS", "TETHYS", "DIONE", "RHEA", "TITAN", "HYPERION", "IAPETUS", "PHOEBE", "SATURN" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." ; bp_scpse.bsp LOG FILE ; ; Created 2008-05-23/13:12:14.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = bp_scpse.bsp INCLUDE_TEXT_FILE = spk_comments_bp_scpse.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/OD/deliveries/080523_068T44/p.nio BODIES = -82 BEGIN_TIME = CAL-ET 2008 MAY 22 13:57:59.900 END_TIME = CAL-ET 2008 JUN 03 12:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/080523_068T44/peph.nio BEGIN_TIME = CAL-ET 2008 MAY 22 13:57:59.900 END_TIME = CAL-ET 2008 JUN 03 12:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/080523_068T44/seph.nio BEGIN_TIME = CAL-ET 2008 MAY 22 13:57:59.900 END_TIME = CAL-ET 2008 JUN 03 12:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.13 $ $Date: 2006/08/18 20:07:20 $ - For OTM-157 based upon OD solution 080523_068T44. This file is invalid after 03-JUN-2008 12:00:00 ET or execution of subsequent maneuvers. This file does not include OTM-157 or its effects. Maneuvers prior to OTM-157 are included. This file includes planetary and satellite ephemerides. This file should only be used in case OTM-157 is NOT implemented. - FILENAME: 080523BP_SCPSE_08144_08155.BSP PURPOSE OF DELIVERY: OTM-157 (MAS ID O157_f) DELIVERY DATE: 080523 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 22-MAY-2008 13:57:59.9 ET SCET END EPOCH OF FILE: 03-JUN-2008 12:00:00 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-157 O157_f By: Cassini-Huygens Navigation Team Profile file: MPF_O157_f_080523_068T44 Maneuver Start: 25-MAY-2008 01:58:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 080523_068T44 -------------------------------------------------------------------------------- DELIVERY NAME: 080523_068T44 BY: Daniel W. Parcher DATE: May 23, 2008 PURPOSE OF DELIVERY: Final OTM157 OD Delivery ORIGINAL DIRECTORY: /cnav/OD/ops/068T44/epoch_080505/otm157/080523 case 4 COMMENTS: Epoch of arc is 5-MAY-2008 12:00:00.000000000 Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat264 and was scaled by a factor of 3 during the T37 data arc and improved with the addition of data through the consecutive arcs leading up to the epoch of this arc. 2-way Doppler and Range through 23-MAY-2008 19:00 Optical Data through 23-MAY-2008 11:59 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 06-MAY-2008 19:30:54.1 SMFDV002 09-MAY-2008 16:21:40.6 SMFDV004 09-MAY-2008 19:36:22.8 SMFDV005 11-MAY-2008 02:55:21.6 SMFDV006 12-MAY-2008 09:20:42.0 SMFDV007 12-MAY-2008 10:38:08.3 SMFDV008 17-MAY-2008 00:53:54.0 SMFDV009 17-MAY-2008 01:59:31.0 SMFDV010 17-MAY-2008 03:24:45.6 SMFDV011 18-MAY-2008 19:32:10.7 SMFDV012 20-MAY-2008 01:59:10.5 SMFDV013 22-MAY-2008 03:27:17.0 MANEUVERS OTM155, ME with Pointing from Telemetry OTM156, RCS with Pointing from Telemetry ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "080523BP_SCPSE_08144_08155.xsp" PRODUCT_CREATION_TIME = 2008-05-23T13:12:28 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-05-22T13:56:55 STOP_TIME = 2008-06-03T11:58:55 SPACECRAFT_CLOCK_START_COUNT = "N/A" SPACECRAFT_CLOCK_STOP_COUNT = "N/A" TARGET_NAME = { "CASSINI", "MERCURY BARYCENTER", "VENUS BARYCENTER", "EARTH BARYCENTER", "MARS BARYCENTER", "JUPITER BARYCENTER", "SATURN BARYCENTER", "URANUS BARYCENTER", "NEPTUNE BARYCENTER", "PLUTO BARYCENTER", "SUN", "MERCURY", "VENUS", "MOON", "EARTH", "MARS", "MIMAS", "ENCELADUS", "TETHYS", "DIONE", "RHEA", "TITAN", "HYPERION", "IAPETUS", "PHOEBE", "SATURN" } INSTRUMENT_NAME = "N/A" INSTRUMENT_ID = "N/A" SOURCE_PRODUCT_ID = "SEE COMMENTS" NOTE = "SPICE transfer format SPK file." \endlabel Brief. Version: 2.2.0 (SPICE Toolkit N0058) Summary for: 080523BP_SCPSE_08144_08155.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2008 MAY 22 13:57:59.900 2008 JUN 03 12:00:00.000 1 MERCURY BARYCENTER Same coverage as previous object 2 VENUS BARYCENTER Same coverage as previous object 3 EARTH BARYCENTER Same coverage as previous object 4 MARS BARYCENTER Same coverage as previous object 5 JUPITER BARYCENTER Same coverage as previous object 6 SATURN BARYCENTER Same coverage as previous object 7 URANUS BARYCENTER Same coverage as previous object 8 NEPTUNE BARYCENTER Same coverage as previous object 9 PLUTO BARYCENTER Same coverage as previous object 10 SUN Same coverage as previous object 199 MERCURY Same coverage as previous object 299 VENUS Same coverage as previous object 301 MOON Same coverage as previous object 399 EARTH Same coverage as previous object 499 MARS Same coverage as previous object 601 MIMAS Same coverage as previous object 602 ENCELADUS Same coverage as previous object 603 TETHYS Same coverage as previous object 604 DIONE Same coverage as previous object 605 RHEA Same coverage as previous object 606 TITAN Same coverage as previous object 607 HYPERION Same coverage as previous object 608 IAPETUS Same coverage as previous object 609 PHOEBE Same coverage as previous object 699 SATURN Same coverage as previous object