MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "080616AP_SCPSE_08168_08217.xsp" PRODUCT_CREATION_TIME = 2008-06-16T14:13:26 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-06-16T14:00:04 STOP_TIME = 2008-08-04T05:58:55 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." ; ap_scpse.bsp LOG FILE ; ; Created 2008-06-16/14:12:58.00. ; ; BEGIN NIOSPK COMMANDS LEAPSECONDS_FILE = /cnav/inputs/naif/latest.tls SPK_FILE = ap_scpse.bsp INCLUDE_TEXT_FILE = spk_comments_ap_scpse.txt INCLUDE_TEXT_FILE = Readme SOURCE_NIO_FILE = /cnav/Man/working/MAS/prime/O159_c/p_with_mvr.nio BODIES = -82 BEGIN_TIME = CAL-ET 2008 JUN 16 14:01:09.000 END_TIME = CAL-ET 2008 AUG 04 06:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/080615_070Sa/peph.nio BEGIN_TIME = CAL-ET 2008 JUN 16 14:01:09.000 END_TIME = CAL-ET 2008 AUG 04 06:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/080615_070Sa/seph.nio BEGIN_TIME = CAL-ET 2008 JUN 16 14:01:09.000 END_TIME = CAL-ET 2008 AUG 04 06:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.14 $ $Date: 2006/08/18 20:07:29 $ - - For OTM-159 based upon OD solution 080615_070Sa. This file is invalid after 4-AUG-2008 06:00:00.0000 ET or execution of subsequent maneuvers. This file accounts for maneuvers up to and including OTM-159. This file includes planetary and satellite ephemerides. - FILENAME: 080616AP_SCPSE_08168_08217.BSP PURPOSE OF DELIVERY: OTM-159 (MAS ID O159_c) DELIVERY DATE: 080616 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 16-JUN-2008 14:01:09.0 ET SCET END EPOCH OF FILE: 4-AUG-2008 06:00:00.0000 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-159 O159_c By: Cassini-Huygens Navigation Team Profile file: MPF_O159_c_080615_070Sa Maneuver Start: 23-JUN-2008 06:24:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 080615_070Sa -------------------------------------------------------------------------------- DELIVERY NAME: 080615_070Sa BY: Shadan Ardalan DATE: June 16, 2008 PURPOSE OF DELIVERY: Preliminary OTM159 OD Delivery ORIGINAL DIRECTORY: /cnav/OD/ops/070Sa/epoch_080520/otm159/080616 case 18 COMMENTS: Epoch of arc is 20-MAY-2008 18:00:00.000000000 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 16-JUN-2008 07:14 Optical Data through 14-JUN-2008 04:49 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 22-MAY-2008 03:27:17.0 SMFDV002 25-MAY-2008 03:49:20.6 SMFDV003 26-MAY-2008 23:35:29.9 SMFDV004 28-MAY-2008 06:35:16.0 SMFDV005 28-MAY-2008 09:02:36.0 SMFDV006 31-MAY-2008 01:41:27.5 SMFDV007 01-JUN-2008 02:10:20.1 SMFDV008 01-JUN-2008 20:31:18.3 SMFDV009 02-JUN-2008 19:06:08.0 SMFDV010 04-JUN-2008 01:15:49.1 SMFDV011 07-JUN-2008 01:01:17.7 SMFDV012 07-JUN-2008 23:34:25.3 SMFDV013 08-JUN-2008 16:43:28.8 SMFDV014 09-JUN-2008 00:35:43.5 SMFDV015 09-JUN-2008 14:47:04.0 SMFDV016 11-JUN-2008 01:02:50.0 SMFDV017 12-JUN-2008 17:42:38.6 SMFDV018 14-JUN-2008 00:44:00.0 SMFDV019 15-JUN-2008 00:34:24.0 MANEUVERS OTM156, RCS (0.197 m/s 22-MAY-2008 02:14) with Pointing from Telemetry OTM157 Cancelled (would have been 25-MAY-2008) OTM158 Cancelled (would have been 01-JUN-2008) ------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "080616AP_SCPSE_08168_08217.xsp" PRODUCT_CREATION_TIME = 2008-06-16T14:13:26 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-06-16T14:00:04 STOP_TIME = 2008-08-04T05:58:55 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: 080616AP_SCPSE_08168_08217.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2008 JUN 16 14:01:09.000 2008 AUG 04 06:00:00.000 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