CCSDS_AEM_VERS = 1.0
CREATION_DATE = 2002-11-04T17:22:31
ORIGINATOR = NASA/JPL

META_START
COMMENT  This file was produced by M.R. Somebody, MSOO NAV/JPL, 2002 OCT 04.
COMMENT  It is to be used for attitude reconstruction only.  The relative accuracy of these
COMMENT   attitudes is 0.1 degrees per axis.
OBJECT_NAME          = MARS GLOBAL SURVEYOR
OBJECT_ID            = 1996-062A
CENTER_NAME          = MARS BARYCENTER
REF_FRAME_A          = EME2000
REF_FRAME_B          = SC_BODY_1
ATTITUDE_DIR         = A2B
TIME_SYSTEM          = UTC
START_TIME           = 1996-11-28T21:29:07.2555
USEABLE_START_TIME   = 1996-11-28T22:08:02.5555
USEABLE_STOP_TIME    = 1996-11-30T01:18:02.5555
STOP_TIME            = 1996-11-30T01:28:02.5555
ATTITUDE_TYPE        = QUATERNION
QUATERNION_TYPE      = LAST
INTERPOLATION_METHOD = HERMITE
INTERPOLATION_DEGREE = 7
META_STOP

DATA_START
1996-11-28T21:29:07.2555 0.56748   0.03146   0.45689   0.68427
1996-11-28T22:08:03.5555 0.42319   -0.45697  0.23784   0.74533
1996-11-28T22:08:04.5555 -0.84532  0.26974   -0.06532  0.45652
1996-11-30T01:28:02.5555  0.74563   -0.45375   0.36875   0.31964
DATA_STOP

META_START
COMMENT   This block begins after trajectory correction maneuver TCM-3.
OBJECT_NAME          = MARS GLOBAL SURVEYOR
OBJECT_ID            = 1996-062A
CENTER_NAME          = MARS BARYCENTER
REF_FRAME_A          = EME2000
REF_FRAME_B          = SC_BODY_1
ATTITUDE_DIR         = A2B
TIME_SYSTEM          = UTC
START_TIME           = 1996-12-18T12:05:00.5555
USEABLE_START_TIME   = 1996-12-18T12:10:00.5555
USEABLE_STOP_TIME    = 1996-12-28T21:23:00.5555
STOP_TIME            = 1996-12-28T21:28:00.5555
ATTITUDE_TYPE        = QUATERNION
QUATERNION_TYPE      = LAST
META_STOP

DATA_START
1996-12-18T12:05:00.5555  -0.64585  0.018542   -0.23854  0.72501
1996-12-18T12:10:05.5555  0.87451   -0.43475   0.13458   -0.16767
1996-12-18T12:10:10.5555  0.03125   -0.65874   0.23458   -0.71418
1996-12-28T21:28:00.5555  -0.25485  0.58745   -0.36845   0.67394
DATA_STOP