<?xml version="1.0" encoding="utf-8"?>
<message xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:noNamespaceSchemaLocation="http://sanaregistry.org/r/ndmxml/ndmxml-1.0-master.xsd"><cdm id="CCSDS_CDM_VERS" version="1.0"><header><COMMENT>CDM_ID:29760445</COMMENT><CREATION_DATE>2020-02-28T19:20:37</CREATION_DATE><ORIGINATOR>JSPOC</ORIGINATOR><MESSAGE_FOR>FENGYUN 2D DEB</MESSAGE_FOR><MESSAGE_ID>000033458_conj_000029163_2020060004017_0591921201</MESSAGE_ID></header><body><relativeMetadataData><TCA>2020-02-29T00:40:17.384</TCA><MISS_DISTANCE units="m">24396</MISS_DISTANCE><RELATIVE_SPEED units="m/s">399</RELATIVE_SPEED><relativeStateVector><RELATIVE_POSITION_R units="m">-6833.4</RELATIVE_POSITION_R><RELATIVE_POSITION_T units="m">-23409.7</RELATIVE_POSITION_T><RELATIVE_POSITION_N units="m">-700.8</RELATIVE_POSITION_N><RELATIVE_VELOCITY_R units="m/s">9.3</RELATIVE_VELOCITY_R><RELATIVE_VELOCITY_T units="m/s">-14.7</RELATIVE_VELOCITY_T><RELATIVE_VELOCITY_N units="m/s">399.2</RELATIVE_VELOCITY_N></relativeStateVector><COLLISION_PROBABILITY/><COLLISION_PROBABILITY_METHOD/><COMMENT>Screening Option = Ellipsoid</COMMENT></relativeMetadataData><segment><metadata><COMMENT>Screened with = inertial state vector.</COMMENT><OBJECT>OBJECT1</OBJECT><OBJECT_DESIGNATOR>33458</OBJECT_DESIGNATOR><CATALOG_NAME>SATCAT</CATALOG_NAME><OBJECT_NAME>FENGYUN 2D DEB</OBJECT_NAME><INTERNATIONAL_DESIGNATOR>2006-053D</INTERNATIONAL_DESIGNATOR><OBJECT_TYPE>DEBRIS</OBJECT_TYPE><OPERATOR_CONTACT_POSITION>https://www.space-track.org/expandedspacedata/query/class/organization/object/~~33458/orderby/ORG_NAME,INFO_ID/format/html/emptyresult/show/</OPERATOR_CONTACT_POSITION><OPERATOR_ORGANIZATION>NONE</OPERATOR_ORGANIZATION><OPERATOR_PHONE>https://www.space-track.org/expandedspacedata/query/class/organization/object/~~33458/orderby/ORG_NAME,INFO_ID/format/html/emptyresult/show/</OPERATOR_PHONE><OPERATOR_EMAIL>https://www.space-track.org/expandedspacedata/query/class/organization/object/~~33458/orderby/ORG_NAME,INFO_ID/format/html/emptyresult/show/</OPERATOR_EMAIL><EPHEMERIS_NAME>NONE</EPHEMERIS_NAME><COVARIANCE_METHOD>CALCULATED</COVARIANCE_METHOD><MANEUVERABLE>N/A</MANEUVERABLE><REF_FRAME>ITRF</REF_FRAME><GRAVITY_MODEL>EGM-96: 8D 8O</GRAVITY_MODEL><ATMOSPHERIC_MODEL>NONE</ATMOSPHERIC_MODEL><N_BODY_PERTURBATIONS>MOON,SUN</N_BODY_PERTURBATIONS><SOLAR_RAD_PRESSURE>YES</SOLAR_RAD_PRESSURE><EARTH_TIDES>NO</EARTH_TIDES><INTRACK_THRUST>NO</INTRACK_THRUST></metadata><data><odParameters><COMMENT>Covariance Scale Factor = 1.000000</COMMENT><COMMENT>Exclusion Volume Radius = 0.000000 [m]</COMMENT><TIME_LASTOB_START>2019-09-01T19:20:37</TIME_LASTOB_START><TIME_LASTOB_END>2020-02-26T19:20:37</TIME_LASTOB_END><RECOMMENDED_OD_SPAN units="d">22.9</RECOMMENDED_OD_SPAN><ACTUAL_OD_SPAN units="d">22.9</ACTUAL_OD_SPAN><OBS_AVAILABLE>123</OBS_AVAILABLE><OBS_USED>123</OBS_USED><RESIDUALS_ACCEPTED units="%">99.2</RESIDUALS_ACCEPTED><WEIGHTED_RMS>1.094</WEIGHTED_RMS></odParameters><additionalParameters><COMMENT>Apogee Altitude = 36110 [km]</COMMENT><COMMENT>Perigee Altitude = 35468 [km]</COMMENT><COMMENT>Inclination = 7.6   [deg]</COMMENT><AREA_PC units="m**2">0.003</AREA_PC><CD_AREA_OVER_MASS units="m**2/kg">0</CD_AREA_OVER_MASS><CR_AREA_OVER_MASS units="m**2/kg">0.1038301179</CR_AREA_OVER_MASS><THRUST_ACCELERATION units="m/s**2">0</THRUST_ACCELERATION><SEDR units="W/kg">0</SEDR></additionalParameters><stateVector><X units="km">19052.114316</X><Y units="km">37955.736441</Y><Z units="km">115.946219</Z><X_DOT units="km/s">0.060414528</X_DOT><Y_DOT units="km/s">-0.038005061</Y_DOT><Z_DOT units="km/s">-0.403423021</Z_DOT></stateVector><covarianceMatrix><COMMENT>DCP Density Forecast Uncertainty = 0.000000000000000E+00</COMMENT><COMMENT>DCP Sensitivity Vector RTN Pos = 0.000000000000000E+00  0.000000000000000E+00  0.000000000000000E+00  [m]</COMMENT><COMMENT>DCP Sensitivity Vector RTN Vel = 0.000000000000000E+00  0.000000000000000E+00  0.000000000000000E+00  [m/sec]</COMMENT><CR_R units="m**2">81324006.02572513</CR_R><CT_R units="m**2">17358237.5907221</CT_R><CT_T units="m**2">84757202.66261144</CT_T><CN_R units="m**2">269811.7386006874</CN_R><CN_T units="m**2">-247526.6901546178</CN_T><CN_N units="m**2">113507.4367949045</CN_N><CRDOT_R units="m**2/s">-3820.67808671728</CRDOT_R><CRDOT_T units="m**2/s">-10903.44878795916</CRDOT_T><CRDOT_N units="m**2/s">287.3309230099815</CRDOT_N><CRDOT_RDOT units="m**2/s**2">5.109617802908433</CRDOT_RDOT><CTDOT_R units="m**2/s">-5937.816740373601</CTDOT_R><CTDOT_T units="m**2/s">-1399.487492335103</CTDOT_T><CTDOT_N units="m**2/s">-18.52604556221489</CTDOT_N><CTDOT_RDOT units="m**2/s**2">0.3048903999665809</CTDOT_RDOT><CTDOT_TDOT units="m**2/s**2">0.433785774454176</CTDOT_TDOT><CNDOT_R units="m**2/s">-270.3655275516757</CNDOT_R><CNDOT_T units="m**2/s">-241.694765776682</CNDOT_T><CNDOT_N units="m**2/s">19.55177152789856</CNDOT_N><CNDOT_RDOT units="m**2/s**2">0.1895815201831259</CNDOT_RDOT><CNDOT_TDOT units="m**2/s**2">0.02043797461529981</CNDOT_TDOT><CNDOT_NDOT units="m**2/s**2">0.009809454326965152</CNDOT_NDOT><CDRG_R units="m**3/kg">0</CDRG_R><CDRG_T units="m**3/kg">0</CDRG_T><CDRG_N units="m**3/kg">0</CDRG_N><CDRG_RDOT units="m**3/(kg*s)">0</CDRG_RDOT><CDRG_TDOT units="m**3/(kg*s)">0</CDRG_TDOT><CDRG_NDOT units="m**3/(kg*s)">0</CDRG_NDOT><CDRG_DRG units="m**4/kg**2">0</CDRG_DRG><CSRP_R units="m**3/kg">0</CSRP_R><CSRP_T units="m**3/kg">0</CSRP_T><CSRP_N units="m**3/kg">0</CSRP_N><CSRP_RDOT units="m**3/(kg*s)">0</CSRP_RDOT><CSRP_TDOT units="m**3/(kg*s)">0</CSRP_TDOT><CSRP_NDOT units="m**3/(kg*s)">0</CSRP_NDOT><CSRP_DRG units="m**4/kg**2">0</CSRP_DRG><CSRP_SRP units="m**4/kg**2">0</CSRP_SRP></covarianceMatrix></data></segment><segment><metadata><COMMENT>Screened with = inertial state vector.</COMMENT><OBJECT>OBJECT2</OBJECT><OBJECT_DESIGNATOR>29163</OBJECT_DESIGNATOR><CATALOG_NAME>SATCAT</CATALOG_NAME><OBJECT_NAME>THAICOM 5</OBJECT_NAME><INTERNATIONAL_DESIGNATOR>2006-020B</INTERNATIONAL_DESIGNATOR><OBJECT_TYPE>PAYLOAD</OBJECT_TYPE><OPERATOR_CONTACT_POSITION>https://www.space-track.org/expandedspacedata/query/class/organization/object/~~29163/orderby/ORG_NAME,INFO_ID/format/html/emptyresult/show/</OPERATOR_CONTACT_POSITION><OPERATOR_ORGANIZATION>THAICOM</OPERATOR_ORGANIZATION><OPERATOR_PHONE>https://www.space-track.org/expandedspacedata/query/class/organization/object/~~29163/orderby/ORG_NAME,INFO_ID/format/html/emptyresult/show/</OPERATOR_PHONE><OPERATOR_EMAIL>https://www.space-track.org/expandedspacedata/query/class/organization/object/~~29163/orderby/ORG_NAME,INFO_ID/format/html/emptyresult/show/</OPERATOR_EMAIL><EPHEMERIS_NAME>NONE</EPHEMERIS_NAME><COVARIANCE_METHOD>CALCULATED</COVARIANCE_METHOD><MANEUVERABLE>N/A</MANEUVERABLE><REF_FRAME>ITRF</REF_FRAME><GRAVITY_MODEL>EGM-96: 8D 8O</GRAVITY_MODEL><ATMOSPHERIC_MODEL>NONE</ATMOSPHERIC_MODEL><N_BODY_PERTURBATIONS>MOON,SUN</N_BODY_PERTURBATIONS><SOLAR_RAD_PRESSURE>YES</SOLAR_RAD_PRESSURE><EARTH_TIDES>NO</EARTH_TIDES><INTRACK_THRUST>NO</INTRACK_THRUST></metadata><data><odParameters><COMMENT>Covariance Scale Factor = 1.000000</COMMENT><COMMENT>Exclusion Volume Radius = 0.000000 [m]</COMMENT><TIME_LASTOB_START>2019-09-01T19:20:37</TIME_LASTOB_START><TIME_LASTOB_END>2020-02-26T19:20:37</TIME_LASTOB_END><RECOMMENDED_OD_SPAN units="d">28.07</RECOMMENDED_OD_SPAN><ACTUAL_OD_SPAN units="d">11.06</ACTUAL_OD_SPAN><OBS_AVAILABLE>2942</OBS_AVAILABLE><OBS_USED>877</OBS_USED><RESIDUALS_ACCEPTED units="%">88.8</RESIDUALS_ACCEPTED><WEIGHTED_RMS>0.863</WEIGHTED_RMS></odParameters><additionalParameters><COMMENT>Apogee Altitude = 36098 [km]</COMMENT><COMMENT>Perigee Altitude = 36082 [km]</COMMENT><COMMENT>Inclination = 0.2   [deg]</COMMENT><AREA_PC units="m**2">34.2637</AREA_PC><CD_AREA_OVER_MASS 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units="m**2/s">-0.7869715257777151</CTDOT_R><CTDOT_T units="m**2/s">0.1322842968842168</CTDOT_T><CTDOT_N units="m**2/s">0.001432378827949391</CTDOT_N><CTDOT_RDOT units="m**2/s**2">-0.00003120098182019067</CTDOT_RDOT><CTDOT_TDOT units="m**2/s**2">0.00005526936175588257</CTDOT_TDOT><CNDOT_R units="m**2/s">-0.003254196412199406</CNDOT_R><CNDOT_T units="m**2/s">0.0068177618489424</CNDOT_T><CNDOT_N units="m**2/s">-0.01176775083782469</CNDOT_N><CNDOT_RDOT units="m**2/s**2">-0.000000529645077499119</CNDOT_RDOT><CNDOT_TDOT units="m**2/s**2">0.0000002242844366352943</CNDOT_TDOT><CNDOT_NDOT units="m**2/s**2">0.000003398167615147133</CNDOT_NDOT><CDRG_R units="m**3/kg">0</CDRG_R><CDRG_T units="m**3/kg">0</CDRG_T><CDRG_N units="m**3/kg">0</CDRG_N><CDRG_RDOT units="m**3/(kg*s)">0</CDRG_RDOT><CDRG_TDOT units="m**3/(kg*s)">0</CDRG_TDOT><CDRG_NDOT units="m**3/(kg*s)">0</CDRG_NDOT><CDRG_DRG units="m**4/kg**2">0</CDRG_DRG><CSRP_R units="m**3/kg">0</CSRP_R><CSRP_T units="m**3/kg">0</CSRP_T><CSRP_N units="m**3/kg">0</CSRP_N><CSRP_RDOT units="m**3/(kg*s)">0</CSRP_RDOT><CSRP_TDOT units="m**3/(kg*s)">0</CSRP_TDOT><CSRP_NDOT units="m**3/(kg*s)">0</CSRP_NDOT><CSRP_DRG units="m**4/kg**2">0</CSRP_DRG><CSRP_SRP units="m**4/kg**2">0</CSRP_SRP></covarianceMatrix></data></segment></body></cdm></message>
