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51989.vcm
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33 lines (33 loc) · 2.02 KB
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<> SP VECTOR/COVARIANCE MESSAGE - V2.0
<>
<> MESSAGE TIME (UTC): 2022 271 (28 SEP) 01:53:56.000 CENTER:
<> SATELLITE NUMBER: 51989 INT. DES.:
<> COMMON NAME:
<> EPOCH TIME (UTC): 2022 270 (27 SEP) 23:09:47.237 EPOCH REV: 3103
<> J2K POS (KM): 4323.67917401 -78.04968046 5389.46854475
<> J2K VEL (KM/S): -1.531172934426 7.320329422891 1.332993163830
<> ECI POS (KM): 4312.23211400 -56.27740403 5398.90281410
<> ECI VEL (KM/S): -1.571287719725 7.312395386472 1.329854429374
<> EFG POS (KM): 4295.62605273 382.24307237 5398.90281410
<> EFG VEL (KM/S): -2.278398950943 6.801614169445 1.329854429374
<> GEOPOTENTIAL: EGM-96 70Z,70T DRAG: JAC70/MSIS90 LUNAR/SOLAR: ON
<> SOLAR RAD PRESS: OFF SOLID EARTH TIDES: ON IN-TRACK THRUST: ON
<> BALLISTIC COEF (M2/KG): 0.631708E-02 BDOT (M2/KG-S): 0.000000E+00
<> SOLAR RAD PRESS COEFF (M2/KG): 0.000000E+00 EDR(W/KG): 0.35E-03
<> THRUST ACCEL (M/S2): 0.100000E-11 C.M. OFFSET (M): 0.000000E+00
<> SOLAR FLUX: F10: 135 AVERAGE F10: 124 AVERAGE AP: 10.0
<> TAI-UTC (S): 37 UT1-UTC (S): -0.00568 UT1 RATE (MS/DAY): 0.237
<> POLAR MOT X,Y (ARCSEC): 0.2822 0.2658 IAU 1980 NUTAT: 4 TERMS
<> TIME CONST LEAP SECOND TIME (UTC): 2049 365 (31 DEC) 23:59:59.999
<> INTEGRATOR MODE: ASW COORD SYS: J2000 PARTIALS: FAST NUM
<> STEP MODE: AUTO FIXED STEP: OFF STEP SIZE SELECTION: MANUAL
<> INITIAL STEP SIZE (S): 20.000 ERROR CONTROL: 0.100E-13
<> VECTOR U,V,W SIGMAS (KM): 0.0176 0.0196 0.0199
<> VECTOR UD,VD,WD SIGMAS (KM/S): 0.0001 0.0000 0.0001
<> COVARIANCE MATRIX (EQUINOCTIAL ELS): ( 7x 7) WTD RMS: 0.12361E+01
<> 0.68605E-11 -0.13751E-10 0.45567E-10 -0.27818E-10 0.92841E-10
<> 0.20355E-09 -0.38091E-12 0.25513E-11 0.67640E-11 0.56558E-12
<> 0.28414E-11 -0.55634E-11 -0.94349E-11 0.80449E-13 0.25560E-11
<> 0.17293E-11 -0.27390E-11 0.55953E-11 0.14305E-11 0.24605E-11
<> 0.13912E-10 -0.15867E-08 0.22052E-07 0.54703E-07 0.42460E-08
<> 0.67308E-09 0.88783E-08 0.98522E-02