CCSDS_OPM_VERS = 2.0
COMMENT Test comment
COMMENT line 2
CREATION_DATE  = 2011-03-01T01:02:03
ORIGINATOR     = ESA

COMMENT Metadata
OBJECT_NAME     = Dragon
OBJECT_ID       = 2010-026A
CENTER_NAME     = EARTH
REF_FRAME       = GCRF
TIME_SYSTEM     = UTC

COMMENT State Vector Components
EPOCH   = 2011-02-24T01:02:03
X       =  149.5345408926215
Y       =   -0.00038977211188
Z       =    0.00149996139666
X_DOT   = 4246.552951206011
Y_DOT   =  -51.94959446834201
Z_DOT   =    0.38290500439795

COMMENT Spacecraft Parameters
MASS            =           2.677682332450020e+17
SOLAR_RAD_AREA  =          16.64382989054804
SOLAR_RAD_COEFF =         132.1620411394343
DRAG_AREA       = 22323254617.47376
DRAG_COEFF      =          64.84786161871301

COMMENT Osculating Keplerian Elements
SEMI_MAJOR_AXIS   =  0.52760862154927
ECCENTRICITY      =  0.9283691897196
INCLINATION       =  0.00100391888685
RA_OF_ASC_NODE    =  3.259238998356167e-05
ARG_OF_PERICENTER =  0.00921403068931
TRUE_ANOMALY      =  0.14285508306175
GM                = 43.20925458951934

COMMENT Position/Velocity Covariance Matrix
CX_X          =               8.663298262953279e-05
CY_X          =               6.73501108282876
CY_Y          =              -2.320970024268873e-12
CZ_X          =              10.67799147417245
CZ_Y          =               2.5340866635355
CZ_Z          =              -0.75822008038839
CX_DOT_X      =               0.06013276699374
CX_DOT_Y      =               0.38608762949737
CX_DOT_Z      = 310498315960961.3
CX_DOT_X_DOT  =              -1.287099387991585e-07
CY_DOT_X      =               0.54873095178357
CY_DOT_Y      =               0.01214075928729
CY_DOT_Z      =   1197926500680.934
CY_DOT_X_DOT  =              -9.671988541187186e-08
CY_DOT_Y_DOT  =        -7844064.954619057
CZ_DOT_X      =              -0.01876857403292
CZ_DOT_Y      =               0.10244118189851
CZ_DOT_Z      =              11.37831353312537
CZ_DOT_X_DOT  =               1.287861812467488e-07
CZ_DOT_Y_DOT  =   -140847421966.4341
CZ_DOT_Z_DOT  =             -16.29733701445678

COMMENT Maneuver Parameters
MAN_EPOCH_IGNITION = 2014-11-12T13:14:15.999999
MAN_DURATION       =      3.780169499126092e-08
MAN_DELTA_MASS     =     -0.00022482802226
MAN_REF_FRAME      = RSW
MAN_DV_1           = 205076.2754452521
MAN_DV_2           =      9.550615917779390e+46
MAN_DV_3           =      0.00018419668559

USER_DEFINED_TEST = 149.53454089262146
USER_DEFINED_TEST2 = String
