CCSDS_OCM_VERS  = 3.0
COMMENT This OCM reflects the latest conditions post-maneuver A67Z
COMMENT This example shows the specification of multiple comment lines
CREATION_DATE         = 1998-11-06T09:23:57
ORIGINATOR            = JAXA
MESSAGE_ID            = OCM 201113719185

META_START
OBJECT_NAME           = OSPREY 5
INTERNATIONAL_DESIGNATOR = 1998-999A

ORIGINATOR_POC        = R. Rabbit
ORIGINATOR_POSITION   = Flight Dynamics Mission Design Lead
ORIGINATOR_PHONE      = (719)555-1234

TECH_POC              = Mr. Rodgers
TECH_PHONE            = (719)555-1234
TECH_ADDRESS          = email@email.XXX

TIME_SYSTEM           = UT1
EPOCH_TZERO           = 1998-12-18T00:00:00.0000

TAIMUTC_AT_TZERO      = 36      [s]
UT1MUTC_AT_TZERO      = .357    [s]
META_STOP

TRAJ_START
COMMENT          GEOCENTRIC, CARTESIAN, EARTH FIXED
COMMENT          THIS IS MY SECOND COMMENT LINE
TRAJ_BASIS            = PREDICTED
TRAJ_REF_FRAME        = EFG
TRAJ_TYPE             = CARTPV
TRAJ_UNITS            = [km, km, km, km/s, km/s, km/s]
1998-12-18T14:28:25.1172 2854.533 -2916.187 -5360.774 5.688 4.652 0.520
TRAJ_STOP

PHYS_START
COMMENT S/C Physical Characteristics:
WET_MASS             = 100.0    [kg]
OEB_Q1               = 0.03123
OEB_Q2               = 0.78543
OEB_Q3               = 0.39158
OEB_QC               = 0.47832
OEB_MAX              = 2.0      [m]
OEB_INT              = 1.0      [m]
OEB_MIN              = 0.5      [m]
AREA_ALONG_OEB_MAX   = 0.15     [m**2]
AREA_ALONG_OEB_INT   = 0.3      [m**2]
AREA_ALONG_OEB_MIN   = 0.5      [m**2]
PHYS_STOP

PERT_START
COMMENT Perturbations Specification:
ATMOSPHERIC_MODEL    = NRLMSIS00
GRAVITY_MODEL        = EGM-96: 36D 36O
GM                   = 398600.4415         [km**3/s**2]
N_BODY_PERTURBATIONS = MOON, SUN
FIXED_GEOMAG_KP      = 12.0
FIXED_F10P7          = 105.0
FIXED_F10P7_MEAN     = 120.0
PERT_STOP

USER_START
USER_DEFINED_CONSOLE_POC = MAXWELL RAFERTY
USER_STOP
