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

META_START
OBJECT_NAME          = OREKIT_SAT
OBJECT_ID            = 2020-012A
CENTER_NAME          = EARTH
REF_FRAME_A          = ITRF-93
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/RATE
QUATERNION_TYPE      = LAST
EULER_ROT_SEQ        = 312
RATE_FRAME           = REF_FRAME_B
INTERPOLATION_METHOD = LINEAR
INTERPOLATION_DEGREE = 1
META_STOP

DATA_START
1996-11-28T21:29:07.255 0.56748   0.03146   0.45689   0.68427    0.001 0.002 0.003
1996-11-28T22:08:03.555 0.42319   -0.45697  0.23784   0.74533    0.004 0.005 0.006
1996-11-28T22:08:05.555 -0.84532  0.26974   -0.06532  0.45652    0.006 0.008 0.009
1996-11-30T01:28:02.555  0.74563   -0.45375   0.36875   0.31964  0.010 0.011 0.012
DATA_STOP