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STS-93 Nominal OMS-2 Orbital Data
- Subject: [sarex] STS-93 Nominal OMS-2 Orbital Data
- From: Ken Ernandes <ken.ernandes@xxxxxxxx>
- Date: Mon, 12 Jul 1999 13:09:31 -0400
Below is the current State Vector and Keplerian Elements for
STS-93. 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 = 10117
Satellite Name: STS-93 OMS-2
Catalog Number: 99993
Epoch MET: 0.03008908565
0/00:43:19.697 MET
EFG E: 9596533.7733649 ft
F: 17258525.1300330 ft
G: -9399732.6040708 ft
Edot: -21545.358129499 ft/s
Fdot: 9134.411962136 ft/s
Gdot: -5217.489150606 ft/s
ndot/2 (drag): 0.00018250050 rev/day^2
nddt/6: 1.39345E-09 rev/day^3
Bstar: 4.42562E-05 1/Earth Radii
Elset #: 1
Rev @ Epoch: 1.67900900186
Launch occurred: 1999-MAY-27 10:49:42.731 UTC
Note that 99993 is a temporary Catalog Number. A permanent Catalog
Number and International Designator will be assigned when STS-93 is
launched.
The following Keplerian elements were computed by VEC2TLE from this
vector, using a 0.5 drag multiplier:
STS-93 OMS-2
1 99993U 99201.22870020 .00018250 13934-8 44256-4 0 14
2 99993 28.4662 199.3456 0003191 302.7331 301.7244 15.95038814 15
Satellite: STS-93 OMS-2
Catalog number: 99993
Epoch time: 99201.22870020
Element set: 1
Inclination: 28.4662 deg
RA of node: 199.3456 deg
Eccentricity: 0.0003191
Arg of perigee: 302.7331 deg
Mean anomaly: 301.7244 deg
Mean motion: 15.95038814 rev/day
Decay rate: 1.82501e-04 rev/day^2
Epoch rev: 1
Checksum: 286
VEC2TLE may be downloaded from <http://www.mindspring.com/~n2wwd>.
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
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