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HB9OK > SAREX 17.04.97 00:46l 102 Lines 4176 Bytes #-10573 (0) @ WW
BID : 447_KCFD
Read: GUEST OE7FMI
Subj: STS-8 Rev 5 Orbital Data
Path: DB0AAB<DB0KCP<DB0KFB<HB9OS<HB9H<HB9OK<IW2FPO<IW5BFZ<IK5CKL<I4UKI<
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From: NWWD@KCFD.#NLI.NY.USA.NA
To : SAREX@AMSAT
STS-8
1 4755U 971A 9796.959114 .1741 791-9 45-4 19
4755 8.468 97.718 75 55.6688 19.14 15.9574 58
Launch time for STS-8: 4 APR 97 @ 19::.88 UTC
Earth-Fixed Greenwich State Vector:
Vector format = 117
Satellite Name: STS-8
Catalog Number: 4755 971A
Epoch Date/Time: 9796.959114
4/6/1997 :1:4.5 UTC
EFG E: 1168. ft
F: -18511886. ft
G: -16646. ft
Edot: 1711.4 ft/s
Fdot: 11541.5 ft/s
Gdot: -19.719999999 ft/s
ndot/ (drag): .174514 rev/day^
nddt/6: 7.917E-1 rev/day^
Bstar: 4.5E-5 1/Earth Radii
Elset #: 1
Rev @ Epoch: 5.5161651
Keplerian Elements (Amsat format):
Satellite: STS-8
Catalog number: 4755
Epoch time: 9796.959114
Element set: 1
Inclination: 8.468 deg
RA of node: 97.718 deg
Eccentricity: .75
Arg of perigee: 55.6688 deg
Mean anomaly: 19.14 deg
Mean motion: 15.9574 rev/day
Decay rate: 1.745e-4 rev/day^
Epoch rev: 5
Checksum: 1
SPACE SHUTTLE ORBITAL DATA:
These -line elements have been generated using Ken Ernandes' program
VECTLE using real time state vector data supplied by DOD C-Band Radar
Network courtesy Dave Simonson. Note that the epoch of the -line
elements is the same as the state vector time.
Drag and B-Star parameters are internally calculated by VECTLE using
a drag factor of .5. Rev numbers use NASA orbit numbering convention.
Dave Ransom
RPV Astronomy BBS
http://www.dransom.com
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