CCSDS_OPM_VERS    = 3.0

COMMENT  Test file for partial maneuver (missing optional fields)

CREATION_DATE     = 2000-06-03T05:33:00.000
ORIGINATOR        = TEST

OBJECT_NAME       = TEST-SAT
OBJECT_ID         = 2000-001A
CENTER_NAME       = EARTH
REF_FRAME         = TOD
TIME_SYSTEM       = UTC

COMMENT  State Vector
EPOCH             = 2006-06-03T00:00:00.000
X                 =   6655.9942        [km]
Y                 = -40218.5751        [km]
Z                 =    -82.9177        [km]
X_DOT             =      3.11548208    [km/s]
Y_DOT             =      0.47042605    [km/s]
Z_DOT             =     -0.00101495    [km/s]

MAN_EPOCH_IGNITION = 2000-06-03T09:00:34.1
MAN_REF_FRAME = J2000
MAN_DV_1 = 0.00101500 [km/s]
MAN_DV_2 = -0.00187300 [km/s]
MAN_DV_3 = 0.00000000 [km/s]
