CCSDS_OCM_VERS            = 3.0

COMMENT  This file is a dummy example with inconsistent data
COMMENT  it is used to exercise all possible keys in Key-Value Notation

CREATION_DATE             = 2019-07-23T10:29:31.576Z
ORIGINATOR                = JPL
MESSAGE_ID                = ABC-12_34

META_START
COMMENT Metadata comment
CLASSIFICATION            = FOUO
OBJECT_NAME               = POLYSAT
INTERNATIONAL_DESIGNATOR  = 2000-053A
CATALOG_NAME              = COMSPOC
OBJECT_DESIGNATOR         = 18SPCS 18571
ALTERNATE_NAMES           = ALTERNATE, OTHER, RELATED
ORIGINATOR_POC            = Mr. Rodgers
ORIGINATOR_POSITION       = Flight Dynamics Mission Design Lead
ORIGINATOR_PHONE          = +12345678901
ORIGINATOR_ADDRESS        = JOHN.DOE@EXAMPLE.ORG
TECH_ORG                  = NASA
TECH_POC                  = Maxwell Smart
TECH_POSITION             = Flight Dynamics Mission Design Lead
TECH_PHONE                = +98765432109
TECH_ADDRESS              = MAX@EXAMPLE.ORG
PREVIOUS_MESSAGE_ID       = ABC-12_33
NEXT_MESSAGE_ID           = ABC-12_35
ADM_MESSAGE_LINK          = ADM-MSG-35132.TXT
CDM_MESSAGE_LINK          = CDM-MSG-35132.TXT
PRM_MESSAGE_LINK          = PRM-MSG-35132.TXT
RDM_MESSAGE_LINK          = RDM-MSG-35132.TXT
TDM_MESSAGE_LINK          = TDM-MSG-35132.TXT
OPERATOR                  = INTELSAT
OWNER                     = SIRIUS
COUNTRY                   = FRANCE
CONSTELLATION             = SPIRE
OBJECT_TYPE               = PAYLOAD
TIME_SYSTEM               = UTC
EPOCH_TZERO               = 2019-07-23T00:00:00
OPS_STATUS                = OPERATIONAL
ORBIT_CATEGORY            = EGO
OCM_DATA_ELEMENTS         = ORBIT, PHYSICAL DESCRIPTION, COVARIANCE, MANEUVER, PERTURBATIONS, OD, USER
SCLK_OFFSET_AT_EPOCH      = 28800 [s]
SCLK_SEC_PER_SI_SEC       = 2.5 [s]
PREVIOUS_MESSAGE_EPOCH    = 2019-07-23T09:29:31.576
NEXT_MESSAGE_EPOCH        = 2019-07-23T11:29:31.576
START_TIME                = 2019-204T09:30:00Z
STOP_TIME                 = 2019-204T10:29:50Z
TIME_SPAN                 = 0.041550925925 [d]
TAIMUTC_AT_TZERO          = 37 [s]
UT1MUTC_AT_TZERO          = -0.1642060 [s]
EOP_SOURCE                = IERS
INTERP_METHOD_EOP         = LAGRANGE_ORDER_5
CELESTIAL_SOURCE          = JPL_DE_430
META_STOP

TRAJ_START
COMMENT                   this is number 1 ORB comment
TRAJ_ID                   = orbit 1
TRAJ_PREV_ID              = orbit 0
TRAJ_NEXT_ID              = orbit 2
TRAJ_BASIS                = DETERMINED_OD
TRAJ_BASIS_ID             = OD_17
INTERPOLATION             = HERMITE
INTERPOLATION_DEGREE      = 3
ORB_AVERAGING             = ECKSTEIN_HECHLER
CENTER_NAME               = EARTH
TRAJ_REF_FRAME            = TOD
TRAJ_FRAME_EPOCH          = 2019-07-23T00:00:00.000
USEABLE_START_TIME        = 2019-204T09:30:00Z
USEABLE_STOP_TIME         = 2019-204T09:59:59.999Z
ORB_REVNUM                = 17
ORB_REVNUM_BASIS          = 1
TRAJ_TYPE                 = CARTPVA
TRAJ_UNITS                = [km,km,km,km/s,km/s,km/s,km/s**2,km/s**2,km/s**2]
  0.0 1000.0 2000.0 3000.0 3.0 2.0 1.0 0.002 -0.003 -0.004
300.0 2000.0 3000.0 4000.0 4.0 3.0 2.0 0.003 -0.004 -0.005
600.0 3000.0 4000.0 5000.0 5.0 4.0 3.0 0.004 -0.005 -0.006
TRAJ_STOP

TRAJ_START
COMMENT                   this is number 2 ORB comment
TRAJ_ID                   = orbit 2
TRAJ_PREV_ID              = orbit 1
TRAJ_NEXT_ID              = orbit 3
TRAJ_BASIS                = PREDICTED
TRAJ_BASIS_ID             = SIMULATION
INTERPOLATION             = LAGRANGE
INTERPOLATION_DEGREE      = 8
ORB_AVERAGING             = OSCULATING
CENTER_NAME               = EARTH
TRAJ_REF_FRAME            = TOD
TRAJ_FRAME_EPOCH          = 2019-07-23T00:00:00.000
USEABLE_START_TIME        = 2019-204T10:00:00Z
USEABLE_STOP_TIME         = 2019-204T10:29:59.999Z
TRAJ_TYPE                 = CARTP
TRAJ_UNITS                = [km,km,km]
1800.0 4000.0 5000.0 6000.0
2100.0 5000.0 6000.0 7000.0
2400.0 6000.0 7000.0 8000.0
TRAJ_STOP

PHYS_START
COMMENT                   this is PHYS comment
MANUFACTURER              = AIRBUS
BUS_MODEL                 = EUROSTAR
DOCKED_WITH               = A1,A2,A3
DRAG_CONST_AREA           = 5            [m**2]
DRAG_COEFF_NOM            = 2.1
DRAG_UNCERTAINTY          = 10.0         [%]
INITIAL_WET_MASS          = 700          [kg]
WET_MASS                  = 600          [kg]
DRY_MASS                  = 500          [kg]
OEB_PARENT_FRAME          = RSW_ROTATING
OEB_PARENT_FRAME_EPOCH    = 2019-204T09:00:00.000Z
OEB_Q1                    = 0.64
OEB_Q2                    = 0.48
OEB_Q3                    = 0.48
OEB_QC                    = 0.36
OEB_MAX                   = 3.0          [m]
OEB_INT                   = 2.0          [m]
OEB_MIN                   = 1.0          [m]
AREA_ALONG_OEB_MAX        = 2.2          [m**2]
AREA_ALONG_OEB_INT        = 3.2          [m**2]
AREA_ALONG_OEB_MIN        = 6.2          [m**2]
AREA_MIN_FOR_PC           = 4.3          [m**2]
AREA_MAX_FOR_PC           = 6.3          [m**2]
AREA_TYP_FOR_PC           = 5.3          [m**2]
RCS                       = 2.4          [m**2]
RCS_MIN                   = 1.4          [m**2]
RCS_MAX                   = 3.4          [m**2]
SRP_CONST_AREA            = 3.5          [m**2]
SOLAR_RAD_COEFF           = 1.7
SOLAR_RAD_UNCERTAINTY     = 20.0         [%]
VM_ABSOLUTE               = 15.0
VM_APPARENT_MIN           = 19.0
VM_APPARENT               = 15.4
VM_APPARENT_MAX           = 14.0
REFLECTIVITY              = 0.7
ATT_CONTROL_MODE          = THREE_AXIS
ATT_ACTUATOR_TYPE         = REACTION_WHEELS
ATT_KNOWLEDGE             = 0.3          [deg]
ATT_CONTROL               = 2.0          [deg]
ATT_POINTING              = 2.3          [deg]
AVG_MANEUVER_FREQ         = 20.0         [#/yr]
MAX_THRUST                = 6.8          [N]
DV_BOL                    = 1.9          [km/s]
DV_REMAINING              = 0.2          [km/s]
IXX                       = 1000.0       [kg*m**2]
IYY                       =  800.0       [kg*m**2]
IZZ                       =  400.0       [kg*m**2]
IXY                       =  20.0        [kg*m**2]
IXZ                       =  40.0        [kg*m**2]
IYZ                       =  60.0        [kg*m**2]
PHYS_STOP

COV_START
COMMENT                   this is number 1 COV comment
COV_ID                    = covariance 1
COV_PREV_ID               = covariance 0
COV_NEXT_ID               = covariance 2
COV_BASIS                 = EMPIRICAL
COV_BASIS_ID              = basis 1
COV_REF_FRAME             = TNW_INERTIAL
COV_FRAME_EPOCH           = 2019-204T09:10:00.000Z
COV_SCALE_MIN             = 0.5
COV_SCALE_MAX             = 5.0
COV_CONFIDENCE            = 25           [%]
COV_TYPE                  = CARTPV
COV_ORDERING              = LTM
COV_UNITS                 = [km,km,km,km/s,km/s,km/s]
  0.0  1.1    2.1  2.2    3.1  3.2  3.3    4.1  4.2  4.3  4.4    5.1  5.2  5.3  5.4  5.5   6.1  6.2  6.3  6.4  6.5  6.6
300.0 11.1   12.1 12.2   13.1 13.2 13.3   14.1 14.2 14.3 14.4   15.1 15.2 15.3 15.4 15.5  16.1 16.2 16.3 16.4 16.5 16.6
600.0 21.1   22.1 22.2   23.1 23.2 23.3   24.1 24.2 24.3 24.4   25.1 25.2 25.3 25.4 25.5  26.1 26.2 26.3 26.4 26.5 26.6
COV_STOP

COV_START
COMMENT                   this is number 2 COV comment
COV_ID                    = covariance 2
COV_PREV_ID               = covariance 1
COV_NEXT_ID               = covariance 3
COV_BASIS                 = SIMULATED
COV_BASIS_ID              = basis 2
COV_REF_FRAME             = TNW_INERTIAL
COV_FRAME_EPOCH           = 2019-204T09:40:00.000Z
COV_SCALE_MIN             = 0.5
COV_SCALE_MAX             = 5.0
COV_CONFIDENCE            = 50           [%]
COV_TYPE                  = CARTPV
COV_ORDERING              = UTMWCC
COV_UNITS                 = [km,km,km,km/s,km/s,km/s]
1800.0 43.0 20.0 3.0 -14.0 -2.0 6.0 0.56636547178859903876 29.0 8.0 2.0 -1.0 16.0 0.15249857033260466633 0.4951875684721383017 9.0 -5.0 0.0 10.0 -0.41087708961862444729 0.071474168989186322187 -0.32075014954979209141 27.0 2.0 3.0 -0.30499714066520933266 -0.18569533817705186314 0. 0.38490017945975050968 1.0 4.0 0.1569197342897824416 0.509543804238785612 0.57166195047502945793 0.099014754297667430918 0.68599434057003534952 34.0
COV_STOP

MAN_START
COMMENT                   this is number 1 MAN comment
MAN_ID                    = maneuver 1
MAN_PREV_ID               = maneuver 0
MAN_NEXT_ID               = maneuver 2
MAN_BASIS                 = DETERMINED_TLM
MAN_BASIS_ID              = TLM 203
MAN_DEVICE_ID             = THR_02
MAN_PREV_EPOCH            = -100.0
MAN_NEXT_EPOCH            = +100.0
MAN_PURPOSE               = ORBIT
MAN_PRED_SOURCE           = OD_5
MAN_REF_FRAME             = TNW_INERTIAL
MAN_FRAME_EPOCH           = 2.3
GRAV_ASSIST_NAME          = MOON
DC_TYPE                   = TIME
DC_WIN_OPEN               = 2.0
DC_WIN_CLOSE              = 100.0
DC_MIN_CYCLES             = 5
DC_MAX_CYCLES             = 30
DC_EXEC_START             = 5.0
DC_EXEC_STOP              = 95.0
DC_REF_TIME               = 8000.0
DC_TIME_PULSE_DURATION    = 10.0          [s]
DC_TIME_PULSE_PERIOD      = 200.0         [s]
MAN_COMPOSITION           = TIME_ABSOLUTE,TIME_RELATIVE,MAN_DURA,DELTA_MASS,ACC_X,ACC_Y,ACC_Z,ACC_INTERP,ACC_MAG_SIGMA,ACC_DIR_SIGMA,DV_X,DV_Y,DV_Z,DV_MAG_SIGMA,DV_DIR_SIGMA,THR_X,THR_Y,THR_Z,THR_EFFIC,THR_INTERP,THR_ISP,THR_MAG_SIGMA,THR_DIR_SIGMA
MAN_UNITS                 = [s,kg,km/s**2,km/s**2,km/s**2,n/a,%,deg,km/s,km/s,km/s,%,deg,N,N,N,n/a,n/a,s,%,deg]
2019-07-23T00:00:00   0.0 200.0 -5.0 0.000734092785 0.000189779834 0.0000794872502 ON 1.0 3.1 0.025 0.0015 0.00029 2.0 5.2 1.0 2.0 3.0 0.95 ON 330.0 2.0 4.3
2019-07-23T00:10:00 600.0 200.0 -5.0 0.000734092785 0.000189779834 0.0000794872502 ON 1.0 3.1 0.025 0.0015 0.00029 2.0 5.2 1.0 2.0 3.0 0.95 ON 330.0 2.0 4.3
MAN_STOP

MAN_START
COMMENT                   this is number 2 MAN comment
MAN_ID                    = maneuver 2
MAN_PREV_ID               = maneuver 1
MAN_NEXT_ID               = maneuver 3
MAN_BASIS                 = PLANNED
MAN_BASIS_ID              = analysis 17
MAN_DEVICE_ID             = THR_07
MAN_PREV_EPOCH            = 200.0
MAN_NEXT_EPOCH            = 300.0
MAN_PURPOSE               = PERIOD
MAN_PRED_SOURCE           = OD_5
MAN_REF_FRAME             = TNW_INERTIAL
MAN_FRAME_EPOCH           = 2.3
GRAV_ASSIST_NAME          = EARTH
DC_TYPE                   = TIME_AND_ANGLE
DC_WIN_OPEN               = 1002.0
DC_WIN_CLOSE              = 1100.0
DC_MIN_CYCLES             = 14
DC_MAX_CYCLES             = 60
DC_EXEC_START             = 1005.0
DC_EXEC_STOP              = 1095.0
DC_REF_TIME               = 12000.0
DC_TIME_PULSE_DURATION    = 20.0             [s]
DC_TIME_PULSE_PERIOD      = 400.0            [s]
DC_REF_DIR                = 1.0 0.0 0.0
DC_BODY_FRAME             = SENSOR_3
DC_BODY_TRIGGER           = 0.707 0.0 0.707
DC_PA_START_ANGLE         = 25.0             [deg]
DC_PA_STOP_ANGLE          = 35.0             [deg]
MAN_COMPOSITION           = TIME_RELATIVE,MAN_DURA,DELTA_MASS,ACC_X,ACC_Y,ACC_Z,ACC_INTERP,ACC_MAG_SIGMA,ACC_DIR_SIGMA,DV_X,DV_Y,DV_Z,DV_MAG_SIGMA,DV_DIR_SIGMA,THR_X,THR_Y,THR_Z,THR_EFFIC,THR_INTERP,THR_ISP,THR_MAG_SIGMA,THR_DIR_SIGMA
MAN_UNITS                 = [s,kg,km/s**2,km/s**2,km/s**2,n/a,%,deg,km/s,km/s,km/s,%,deg,N,N,N,n/a,n/a,s,%,deg]
1000.0 200.0 -5.0 0.000734092785 0.000189779834 0.0000794872502 OFF 1.0 3.1 0.025 0.0015 0.00029 2.0 5.2 1.0 2.0 3.0 0.95 ON 330.0 2.0 4.3
1600.0 200.0 -5.0 0.000734092785 0.000189779834 0.0000794872502 OFF 1.0 3.1 0.025 0.0015 0.00029 2.0 4.2 1.0 2.0 3.0 0.95 ON 330.0 2.0 4.3
MAN_STOP

MAN_START
COMMENT                   this is number 3 MAN comment
MAN_ID                    = maneuver 3
MAN_DEVICE_ID             = DEPLOYMENT
MAN_COMPOSITION           = TIME_ABSOLUTE,DEPLOY_ID,DEPLOY_DV_X,DEPLOY_DV_Y,DEPLOY_DV_Z,DEPLOY_MASS,DEPLOY_DV_SIGMA,DEPLOY_DIR_SIGMA,DEPLOY_DV_RATIO,DEPLOY_DV_CDA
MAN_UNITS                 = [n/a,km/s,km/s,km/s,kg,%,deg,n/a,m**2]
2019-07-23T09:45:00 BEE_1  0.0001  0.0003  0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:46:00 BEE_2  0.0001  0.0003 -0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:47:00 BEE_3  0.0001 -0.0003  0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:48:00 BEE_4  0.0001 -0.0003 -0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:49:00 BEE_5 -0.0001  0.0003  0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:50:00 BEE_6 -0.0001  0.0003 -0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:51:00 BEE_7 -0.0001 -0.0003  0.0002 -0.4 5.0 7.2 -0.05 0.022
2019-07-23T09:52:00 BEE_8 -0.0001 -0.0003 -0.0002 -0.4 5.0 7.2 -0.05 0.022
MAN_STOP

PERT_START
COMMENT                   this is PERT comment
ATMOSPHERIC_MODEL         = NRLMSIS00
GRAVITY_MODEL             = TEG-4: 36D 12O
EQUATORIAL_RADIUS         = 6378.137           [km]
GM                        = 398600.4415        [km**3/s**2]
N_BODY_PERTURBATIONS      = MOON,SUN
CENTRAL_BODY_ROTATION     = 4.17807421629e-3   [deg/s]
OBLATE_FLATTENING         = 0.00335281066475
OCEAN_TIDES_MODEL         = SEMI-DIURNAL
SOLID_TIDES_MODEL         = DIURNAL
REDUCTION_THEORY          = IERS2010
ALBEDO_MODEL              = KNOCKE
ALBEDO_GRID_SIZE          = 100
SHADOW_MODEL              = DUAL CONE
SHADOW_BODIES             = EARTH,MOON
SRP_MODEL                 = BOX_WING
SW_DATA_SOURCE            = CELESTRAK
SW_DATA_EPOCH             = 2019-07-22T00:00:00.000
SW_INTERP_METHOD          = LAGRANGE_ORDER_5
FIXED_GEOMAG_KP           = 3.2                [nT]
FIXED_GEOMAG_AP           = 2.1                [nT]
FIXED_GEOMAG_DST          = -20                [nT]
FIXED_F10P7               = 120.0              [SFU]
FIXED_F10P7_MEAN          = 132.0              [SFU]
FIXED_M10P7               = 130.0              [SFU]
FIXED_M10P7_MEAN          = 142.0              [SFU]
FIXED_S10P7               = 140.0              [SFU]
FIXED_S10P7_MEAN          = 152.0              [SFU]
FIXED_Y10P7               = 150.0              [SFU]
FIXED_Y10P7_MEAN          = 162.0              [SFU]
PERT_STOP

OD_START
COMMENT                   this is OD comment
OD_ID                     = OD_24
OD_PREV_ID                = OD_23
OD_METHOD                 = BWLS: OREKIT
OD_EPOCH                  = 2019-07-22T17:32:27
DAYS_SINCE_FIRST_OBS      = 3.5                 [d]
DAYS_SINCE_LAST_OBS       = 1.2                 [d]
RECOMMENDED_OD_SPAN       = 5.2                 [d]
ACTUAL_OD_SPAN            = 2.3                 [d]
OBS_AVAILABLE             = 100
OBS_USED                  =  90
TRACKS_AVAILABLE          =  33
TRACKS_USED               =  30
MAXIMUM_OBS_GAP           = 1.0                 [d]
OD_EPOCH_EIGMAJ           = 58.73               [m]
OD_EPOCH_EIGMED           = 35.7                [m]
OD_EPOCH_EIGMIN           = 21.5                [m]
OD_MAX_PRED_EIGMAJ        = 32.5                [m]
OD_MIN_PRED_EIGMIN        = 22.0                [m]
OD_CONFIDENCE             = 95.3                [%]
GDOP                      = .857
SOLVE_N                   = 6
SOLVE_STATES              = POS[3], VEL[3]
CONSIDER_N                = 2
CONSIDER_PARAMS           = DRAG, SRP
SENSORS_N                 = 3
SENSORS                   = EGLIN,FYLINGDALES,PLAGNOLE
WEIGHTED_RMS              = 1.3
DATA_TYPES                = RANGE,DOPPLER,AZEL
OD_STOP

USER_START
COMMENT                   this is USER comment
USER_DEFINED_LIBRARY      = OREKIT
USER_STOP

