N2WWD > SAREX 13.07.97 20:54l 64 Lines 1878 Bytes #-10398 (0) @ AMSAT
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Subj: STS-94 Rev 129 Orbital Data
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From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
To : SAREX@AMSAT
Below is the current State Vector and Keplerian Elements for
STS-94. The vector data comes from NASA; the Keplerian Elements
were computed from the vector.
This file may be read by VEC2TLE version 9648 to update your
Keplerian Elements text file.
Vector format = 117
Satellite Name: STS-94
Catalog Number: 24849 97032A
Epoch Date/Time: 97190.79203935200
07/09/1997 19:00:32.200 UTC
EFG E: -11725131.000000 ft
F: -16279951.000000 ft
G: 8755190.00000000 ft
Edot: 16877.7200000000 ft/s
Fdot: -15714.780000000 ft/s
Gdot: -6567.9399999999 ft/s
ndot/2 (drag): 0.00056547316 rev/day^2
nddt/6: 1.34153E-08 rev/day^3
Bstar: 1.73462E-04 1/Earth Radii
Elset #: 34
Rev @ Epoch: 129.34124207447
Launch: 01-JUL-97 / 18:02:00.063 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector and the scheduled launch time using a 2.0 drag multiplier:
STS-94
1 24849U 97032A 97190.79203935 .00056547 13415-7 17346-3 0 344
2 24849 28.4687 320.7700 0004537 61.2839 61.5465 15.90578398 1295
Satellite: STS-94
Catalog number: 24849
Epoch time: 97190.79203935
Edment set: 34
Inclination: 28.4687 deg
RA of node: 320.7700 deg
Eccentricity: 0.0004537
Arg of perigee: 61.2839 deg
Mean anomaly: 61.5465 deg
Mean motion: 15.90578398 rev/day
Decay rate: 5.65473e-04 rev/day^2
Epoch rev: 129
Checksum: 345
VEC2TLE may be downloaded from:
http://www.amsat.org/amsat/sarex/orbit.html
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
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