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OD5NZ > SAREX 09.03.96 23:27l 60 Lines 1838 Bytes #-11082 (0) @ AMSAT
BID : 51_OD5NZ
Read: OE5GMM DF5CH GUEST OE7FMI
Subj: STS-75 Rev 203 Orbital Data
Path: DB0AAB<DB0FSG<DB0IGL<DB0KCP<HB9OS<HB9H<HB9OK<IW2FPO<IK2QCA<I3NXU<
IW4CNQ<IK6LJP<LY1BZB<OD5RAK<OD5ET<OD5KU<OD5NZ
Sent: 960307/2109z @:OD5NZ.AMPR.ORG [Beirut, KM73SV] TCP/IP <> AX.25 Gateway #:
S T S - 7 5 O R B I T A L D A T A
Below is the rev 203 Earth-Fixed Greenwich (EFG) state vector for
STS-75. This vector data comes from NASA GSFC and was provided
courtesy of the DOD C-Band Radar Network.
Vector format = 117
Satellite Name: STS-75
Catalog Number: 23801 96012A
Epoch Date/Time: 96066.54391435185
03/06/1996 13:03:14.200 UTC
EFG E: -21748058 ft
F: -446936 ft
G: -2083504 ft
Edot: -684.41 ft/s
Fdot: -20856.30 ft/s
Gdot: 11858.53 ft/s
ndot/2 (drag): 0.00000855790 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 1.81670E-06 1/Earth Radii
Elset #: 31
Rev @ Epoch: 203.96823095976
Launch was 22-FEB-96 / 20:17:59.968 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.02 drag multiplier:
STS-75
1 23801U 96012A 96066.54391435 .00000856 00000-0 18167-5 0 317
2 23801 28.4462 191.7176 0005211 113.9081 234.6479 15.97440497 2036
Satellite: STS-75
Catalog number: 23801
Epoch time: 96066.54391435
Element set: 31
Inclination: 28.4462 deg
RA of node: 191.7176 deg
Eccentricity: 0.0005211
Arg of perigee: 113.9081 deg
Mean anomaly: 234.6479 deg
Mean motion: 15.97440497 rev/day
Decay rate: 8.55790e-06 rev/day^2
Epoch rev: 203
Checksum: 315
The next release of VEC2TLE will provide a feature to automatically
update your TLE or AMSAT Keplerian element file(s).
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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