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STS-92 Nominal OMS-2 Orbital Data
- Subject: [sarex] STS-92 Nominal OMS-2 Orbital Data
- From: "Kenneth J. Ernandes" <n2wwd@xxxxxxxxxxxxxx>
- Date: Wed, 27 Sep 2000 14:11:09 -0400
Below is the nominal State Vector and Keplerian Elements for
STS-92. 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-92
Catalog Number: 99992
Epoch MET: 0.03388303241
0/00:48:47.494 MET
EFG E: 1631791.393471 ft
F: 19762741.827654 ft
G: -9449969.492566 ft
Edot: -16521.230762 ft/s
Fdot: -6592.979646 ft/s
Gdot: -16498.961429 ft/s
ndot/2 (drag): 0.00039546673 rev/day^2
nddt/6: 6.51424E-09 rev/day^3
Bstar: 5.39629E-05 1/Earth Radii
Elset #: 1
Rev @ Epoch: 1.59327298595
Launch Scheduled: 2000-OCT-06 0138:38 UTC
Note that 99992 is a temporary Catalog Number. A permanent Catalog
Number and International Designator will be assigned when STS-92 is
launched.
The following Keplerian elements were computed by VEC2TLE from this
vector, using a 0.5 drag multiplier:
STS-92
1 99992U 00280.10237840 .00039547 65142-8 53963-4 0 11
2 99992 51.5770 294.9715 0068674 8.7269 204.8296 16.00722458 12
Satellite: STS-92
Catalog number: 99992
Epoch time: 00280.10237840
Element set: 1
Inclination: 51.5770 deg
RA of node: 294.9715 deg
Eccentricity: 0.0068674
Arg of perigee: 8.7269 deg
Mean anomaly: 204.8296 deg
Mean motion: 16.00722458 rev/day
Decay rate: 3.95467e-04 rev/day^2
Epoch rev: 1
Checksum: 319
VEC2TLE may be downloaded from <http://www.mindspring.com/~n2wwd>.
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
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