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N2WWD > SAREX 22.08.97 22:59l 62 Lines 1846 Bytes #-10355 (0) @ AMSAT
BID : 46999_KC2FD
Read: GUEST OE7FMI
Subj: STS-85 Rev 99 Orbital Data
Path: DB0RGB<DB0MAK<DB0ERF<DB0SAW<DB0HRO<DB0OQ<DB0IL<OZ5BBS<OZ4PAC<OZ4BBS<
OZ3PAC<OZ6BBS<SK7CY<SK6FV<SK6YW<SK6BA<SK6LK<SM7FEJ<SK7HR<SK5AS<SK5BN<
SK5UM<SK5AE<SK0MK<SK0QO<SM0GJK<OH0RBA<OH1RBU<OH7RBA<VK3ECV<N1KIO<
WU3V<WB0TAX<KE2VW<W2IM<KB2FAF<KA3VRW<N3DPU<WB3FYL<K3PGB<WA3TSW<K2ADJ<
WT3V<KC2PB<WB2COP<WA2SNA<KB2VLX<N2BQF<KC2FD
Sent: 970814/0122Z @:KC2FD.#NLI.NY.USA.NA #:46999 [Coram_LI] $:46999_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To : SAREX@AMSAT
Below is the current State Vector and Keplerian Elements for
STS-85. 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-85
Catalog Number: 24889 97039A
Epoch Date/Time: 97225.83407754600
08/13/1997 20:01:04.299 UTC
EFG E: -11207126.000000 ft
F: -6229409.0000000 ft
G: 17713107.0000000 ft
Edot: 17625.8100000000 ft/s
Fdot: -16103.430000000 ft/s
Gdot: 5500.18999999999 ft/s
ndot/2 (drag): 0.00034896891 rev/day^2
nddt/6: 5.09194E-09 rev/day^3
Bstar: 9.09206E-05 1/Earth Radii
Elset #: 25
Rev @ Epoch: 99.20831074248
Launch: 07-AUG-97 / 14:41:00.082 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector, using a 1.0 drag multiplier:
STS-85
1 24889U 97039A 97225.83407755 .00034897 50919-8 90921-4 0 251
2 24889 56.9973 47.7440 0009409 311.8427 123.1330 15.94276887 994
Satellite: STS-85
Catalog number: 24889
Epoch time: 97225.83407755
Element set: 25
Inclination: 56.9973 deg
RA of node: 47.7440 deg
Eccentricity: 0.0009409
Arg of perigee: 311.8427 deg
Mean anomaly: 123.1330 deg
Mean motion: 15.94276887 rev/day
Decay rate: 3.48969e-04 rev/day^2
Epoch rev: 99
Checksum: 363
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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