MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "080228AP_SCPSE_08050_08076.xsp" PRODUCT_CREATION_TIME = 2008-02-28T11:03:22 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-02-19T18:58:55 STOP_TIME = 2008-03-16T05:58:55 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 2008-02-28/11:02:56.00. ; ; 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/offline/prime/O146_k/p_with_mvr.nio BODIES = -82 BEGIN_TIME = CAL-ET 2008 FEB 19 19:00:00.000 END_TIME = CAL-ET 2008 MAR 16 06:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/080228_060E3/peph.nio BEGIN_TIME = CAL-ET 2008 FEB 19 19:00:00.000 END_TIME = CAL-ET 2008 MAR 16 06:00:00.000 SOURCE_NIO_FILE = /cnav/OD/deliveries/080228_060E3/seph.nio BEGIN_TIME = CAL-ET 2008 FEB 19 19:00:00.000 END_TIME = CAL-ET 2008 MAR 16 06:00:00.000 ; END NIOSPK COMMANDS % template version $Revision: 1.14 $ $Date: 2006/08/18 20:07:29 $ - - For OTM-146 based upon OD solution 080228_060E3. This file is invalid after 16-MAR-2008 06:00:00 ET or execution of subsequent maneuvers. This file accounts for maneuvers up to and including OTM-146. This file includes planetary and satellite ephemerides. - FILENAME: 080228AP_SCPSE_08050_08076.BSP PURPOSE OF DELIVERY: OTM-146 (MAS ID O146_k) DELIVERY DATE: 080228 PLANETARY EPHEMERIS USED: from OD delivery SATELLITE/ASTEROID/ROCK EPHEMERIS USED: from OD delivery START EPOCH OF FILE: 19-FEB-2008 19:00:00 ET SCET END EPOCH OF FILE: 16-MAR-2008 06:00:00 ET SCET ------ COMMENTS FROM NAV/MVR FOR OTM-146 O146_k By: Cassini-Huygens Navigation Team Profile file: MPF_O146_k_080228_060E3 Maneuver Start: 01-MAR-2008 22:56:00.000 UTC SCET ------ COMMENTS FROM NAV/OD FOR DELIVERY 080228_060E3 -------------------------------------------------------------------------------- DELIVERY NAME: 080228_060E3 BY: Daniel W. Parcher DATE: February 28, 2008 PURPOSE OF DELIVERY: Final OD Delivery for OTM146 ORIGINAL DIRECTORY: /cnav/OD/ops/060E3/epoch_080214/otm146/080228_dwp case 5 COMMENTS: Epoch of arc is 14-FEB-2008 18:00:00.000000000 Spacecraft a priori state and covariance from sat282 delivery Spacecraft State covariance with scale factor of 5 Satellite/planet Covariance sat282 2-way Doppler and Range through 28-FEB-2008 12:02 Optical Data through 15-FEB-2008 02:20 Weights by pass for F2 and SRA SMALL FORCES: SMFDV001 16-FEB-2008 07:43:09.3 SMFDV002 17-FEB-2008 08:58:05.5 SMFDV003 19-FEB-2008 07:56:48.6 SMFDV004 19-FEB-2008 09:32:51.9 SMFDV005 19-FEB-2008 23:04:48.3 SMFDV006 21-FEB-2008 06:10:28.9 SMFDV008 21-FEB-2008 10:13:16.4 SMFDV009 22-FEB-2008 16:50:51.0 SMFDV010 22-FEB-2008 19:01:16.2 MANEUVERS OTM145 Estimated with Telemetry Values and Unweighted Uncertainties ------------------------------------------------------------------------------------- \beginlabel MISSION_NAME = "CASSINI" SPACECRAFT_NAME = "CASSINI" DATA_SET_ID = "SPICE_SPK_FILE" KERNEL_TYPE_ID = "SPK" PRODUCT_ID = "080228AP_SCPSE_08050_08076.xsp" PRODUCT_CREATION_TIME = 2008-02-28T11:03:22 PRODUCER_ID = "CASSINI_NAV" MISSION_PHASE_NAME = "TOUR" PRODUCT_VERSION_TYPE = "PREDICT" PLATFORM_OR_MOUNTING_NAME = "N/A" START_TIME = 2008-02-19T18:58:55 STOP_TIME = 2008-03-16T05:58:55 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: 080228AP_SCPSE_08050_08076.bsp Bodies Start of Interval (ET) End of Interval (ET) ------- ----------------------------- ----------------------------- -82 CASSINI 2008 FEB 19 19:00:00.000 2008 MAR 16 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