MISSION_NAME             = CASSINI
SPACECRAFT_NAME          = CASSINI
DATA_SET_ID              = SPICE_SPK_FILE
KERNEL_TYPE_ID           = SPK
PRODUCT_ID               = 000202R_SK_V2P12_EP15.XSP
PRODUCT_CREATION_TIME    = 1999-09-24T11:21:08
PRODUCER_ID              = CASSINI_NAV_TEAM
MISSION_PHASE_NAME       = 'VENUS 2 TO EARTH'
PRODUCT_VERSION_TYPE     = 'FINAL RECONST TRAJ'
PLATFORM_OR_MOUNTING_NAME = N/A
START_TIME               = 1999-07-06T16:00:00
STOP_TIME                = 1999-09-02T12:00:00
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: 000202R_SK_V2P12_EP15.XSP
 
PURPOSE OF DELIVERY: Final, archival trajectory reconstruction for Cassini
                     for the period from Venus 2 to Earth.
 
DELIVERED BY: Fernando Peralta 3-0528. The original nio file was produced
              by Mark Guman.
 
DELIVERY DATE: February 2, 2000
 
FILE USAGE RESTRICTIONS: None
 
PLANETARY EPHEMERIS USED: DE405
 
SATELLITE/ASTEROID/ROCK EPHEMERIS USED: N/A
 
START EPOCH OF PROPAGATED DATA ARC: N/A
 
END EPOCH OF PROPAGATED DATA ARC: N/A
 
START EPOCH OF RECONSTRUCTED DATA ARC: 6 JULY 1999 16:00:00 UTC.
 
END EPOCH OF RECONSTRUCTED DATA ARC: 2 SEPTEMBER 1999 12:00:00 UTC.
 
COMMENTS:
 
2-way Doppler (0.2 mm/s) and range (10 m) solution with data from
26 June 1999 to 2 September 99.  Estimate s/c state, solar pressure (component
model), solar torque, RTG radiation, 11 impulsive delta-Vs (deadband resets
for TCM-9, TCM-10, TCM-11, TCM-12 and TCM-13, VIMS cover release, mag boom
deployment, pre-Earth roll, pre-Earth deadband reset, Earth flyby gravity
gradient DV, and post-Earth roll), maneuver parameters (DV, RA, DEC, Start
Time) for TCM-9 TCM-10, TCM-11, TCM-12 and TCM-13, post-maneuver exponential
accelerations for TCM-9, TCM-10, TCM-11, TCM-12 and TCM-13, post mag boom
deployment exponential acceleration, and Earth-Moon barycenter ephemeris.
Niell tropospheric refraction model used.
 
Uncertainty ellipse has been scaled such that the semi-major axis is 30 m.
 
 
Brief.  Version: 2.1        (SPICE Toolkit N0051)
 
 
Summary for: 000202R_SK_V2P12_EP15.bsp
 
Bodies       Start of Interval (ET)          End of Interval (ET)
-------      -----------------------------   -----------------------------
-82 CASSINI  1999 JUL 06 16:01:04.183        1999 SEP 02 12:01:04.182