HR1RBB > SAREX 27.05.96 02:14l 62 Lines 1763 Bytes #-11002 (0) @ AMSAT
BID : 17526_HR1PAQ
Read: GUEST OE7FMI
Subj: STS-77 Rev 98 Orbital Data
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Sent: 960525/2252Z @:HR1PAQ.#TGU.HON.CEAM #:17526 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-77 Rev 98 Orbital Data
S T S - 7 7 O R B I T A L D A T A
Below is the rev 98 Earth-Centered Inertial (ECI) state vector for
STS-77. This vector data comes from NASA GSFC OIG RAID RBBS.
Vector format = 117
Satellite Name: STS-77
Catalog Number: 23870 96032A
Epoch Date/Time: 96146.50126620370
05/25/1996 12:01:49.399 UTC
EFG E: -21283953.0 ft
F: -1739222.0 ft
G: 4573465.0 ft
Edot: 4740.44 ft/s
Fdot: -18300.83 ft/s
Gdot: 15087.98 ft/s
ndot/2 (drag): 0.00005037792 rev/day^2
nddt/6: 1.05998E-10 rev/day^3
Bstar: 1.09462E-05 1/Earth Radii
Elset #: 19
Rev @ Epoch: 98.05398940366
Launch was 19-MAY-96 / 10:30:00.080 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.12 drag multiplier:
STS-77
1 23870U 96032A 96146.50126620 .00005038 10600-9 10946-4 0 197
2 23870 39.0143 233.1377 0007102 306.6959 72.7406 15.97186442 986
Satellite: STS-77
Catalog number: 23870
Epoch time: 96146.50126620
Element set: 19
Inclination: 39.0143 deg
RA of node: 233.1377 deg
Eccentricity: 0.0007102
Arg of perigee: 306.6959 deg
Mean anomaly: 72.7406 deg
Mean motion: 15.97186442 rev/day
Decay rate: 5.03779e-05 rev/day^2
Epoch rev: 98
Checksum: 316
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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