MISSION_NAME             = CASSINI
SPACECRAFT_NAME          = CASSINI
DATA_SET_ID              = SPICE_SPK_FILE
KERNEL_TYPE_ID           = SPK
PRODUCT_ID               = 000331_SK_JM229_SP0.XSP
PRODUCT_CREATION_TIME    = 2000-03-30T14:32:14
PRODUCER_ID              = CASSINI_NAV_TEAM
MISSION_PHASE_NAME       = 'JUP - 229d to SOI'
PRODUCT_VERSION_TYPE     = 'REFERENCE TRAJECTORY'
PLATFORM_OR_MOUNTING_NAME = N/A
START_TIME               = 2000-05-15T00:00:00
STOP_TIME                = 2004-07-01T12:00:00
SPACECRAFT_CLOCK_START_COUNT = N/A
SPACECRAFT_CLOCK_STOP_COUNT = N/A
TARGET_NAME              = CASSINI
INSTRUMENT_NAME          = N/A
INSTRUMENT_ID            = N/A
SOURCE_PRODUCT_ID        = UNK
NOTE                     = 'SPICE transfer format SPK file.'
 
FILENAME: 000331_SK_JM229_SP0.XSP
 
PURPOSE OF DELIVERY: This delivery of the reference trajectory includes
                     TCM-14, TCM-17, TCM-18, and TCM-19. The Phoebe flyby
                     is also included as well as the Phoebe minus 15 day
                     maneuver. No more than 400 days pass without a firing
                     of at least 5 seconds. The trajectory is also targeted
                     to have the appropriate ring crossing.
 
DELIVERED BY: Fernando Peralta. The Reference Trajectory was generated by
              Troy Goodson.
 
DELIVERY DATE: March 31,2000.
 
FILE USAGE RESTRICTIONS: DO NOT USE THIS TRAJECTORY BEFORE MAY 15, 2000.
                         THIS TRAJECTORY DOES NOT INCLUDE SOI.
 
PLANETARY EPHEMERIS USED: DE405, SAT105, and JUP100.
 
SATELLITE/ASTEROID/ROCK EPHEMERIS USED: N/A
 
START EPOCH OF PROPAGATED DATA ARC: MAY 15, 2000 00:00:00 UTC.
 
END EPOCH OF PROPAGATED DATA ARC: JULY 1, 2004 12:00:00 UTC.
 
START EPOCH OF RECONSTRUCTED DATA ARC: N/A.
 
END EPOCH OF RECONSTRUCTED DATA ARC: N/A.
 
COMMENTS:
 
COMPARISON BETWEEN THIS DELIVERY (000331) AND THE PREVIOUS REFERENCE TRAJECTORY (990803).
 
                         000331                  990803         DIFFERENCE
                         ------                  ------         ----------
 
START (ET)         15-MAY-2000 00:00:00   26-JUN-1999 14:00:00
JUPITER TCA (UTC)  30-DEC-2000 10:03:39   30-DEC-2000 10:07:09  3 min 10 sec
        B.R (km)       123,623                130,523               6900
        B.T (km)    10,897,196             10,898,129                933
SATURN  TCA (UTC)   1-JUL-2004 02:36:48    1-JUL-2004 02:36:35       -13 sec
        B.R (km)      -189,313               -187,880               1433
        B.T (km)       416,757                416,086               -671
END (ET)            1-JUL-2004 12:00:00    1-JUL-2004 12:00:00
 
PHOEBE TCA  (UTC)  11-JUN-2004 20:22:03
  ALTITUDE   (km)         2000
       B.R   (km)         -874
       B.T   (km)         1921
 
NOTE: All B-plane quantities are given with respect to EMO2000. The Jupiter
B-plane quantities are bary-centered, and the Saturn B-plane quantities are
planet-centered.
 
 
Brief.  Version: 2.1        (SPICE Toolkit N0051)
 
 
Summary for: 000331_SK_JM229_SP0.bsp
 
Bodies       Start of Interval (ET)          End of Interval (ET)
-------      -----------------------------   -----------------------------
-82 CASSINI  2000 MAY 15 00:00:00.000        2004 JUL 01 12:00:00.000