N2WWD > SAREX 13.07.97 20:59l 64 Lines 1879 Bytes #-10398 (0) @ AMSAT
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Subj: STS-94 Rev 145 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: 97191.79435879600
07/10/1997 19:03:52.599 UTC
EFG E: -15934281.000000 ft
F: -11630079.000000 ft
G: 9476473.00000000 ft
Edot: 11776.3500000000 ft/s
Fdot: -20272.400000000 ft/s
Gdot: -5041.4700000000 ft/s
ndot/2 (drag): 0.00057103082 rev/day^2
nddt/6: 1.36792E-08 rev/day^3
Bstar: 1.74008E-04 1/Earth Radii
Elset #: 38
Rev @ Epoch: 145.31833238155
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 97191.79435880 .00057103 13679-7 17401-3 0 388
2 24849 28.4689 313.2762 0004546 70.3271 44.2587 15.90707223 1455
Satellite: STS-94
Catalog number: 24849
Epoch time: 97191.79435880
Element set: 38
Inclination: 28.4689 deg
RA of node: 313.2762 deg
Eccentricity: 0.0004546
Arg of perigee: 70.3271 deg
Mean anomaly: 44.2587 deg
Mean motion: 15.90707223 rev/day
Decay rate: 5.71031e-04 rev/day^2
Epoch rev: 145
Checksum: 323
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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