HR1RBB > SAREX 05.06.96 06:01l 63 Lines 1808 Bytes #-10992 (0) @ AMSAT
BID : 17828_HR1PAQ
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Subj: STS-77 Rev 146 Orbital Data
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Sent: 960529/0358Z @:HR1PAQ.#TGU.HON.CEAM #:17828 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-77 Rev 146 Orbital Data
S T S - 7 7 O R B I T A L D A T A
Below is the rev 146 Earth-Fixed Greenwich (EFG) state vector for
STS-77. This vector data comes from NASA GSFC and was provided
courtesy of the DOD C-Band Radar Network.
Vector format = 117
Satellite Name: STS-77
Catalog Number: 23870 96032A
Epoch Date/Time: 96149.50210532407
05/28/1996 12:03:01.899 UTC
EFG E: -20352628 ft
F: 5880820 ft
G: 5244951 ft
Edot: -1695.03 ft/s
Fdot: -19076.26 ft/s
Gdot: 14793.80 ft/s
ndot/2 (drag): 0.00005330773 rev/day^2
nddt/6: 1.18631E-10 rev/day^3
Bstar: 1.11095E-05 1/Earth Radii
Elset #: 30
Rev @ Epoch: 146.06237289643
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 96149.50210532 .00005331 11863-9 11110-4 0 301
2 23870 39.0141 213.1422 0008120 332.2170 50.2375 15.97917509 1460
Satellite: STS-77
Catalog number: 23870
Epoch time: 96149.50210532
Element set: 30
Inclination: 39.0141 deg
RA of node: 213.1422 deg
Eccentricity: 0.0008120
Arg of perigee: 332.2170 deg
Mean anomaly: 50.2375 deg
Mean motion: 15.97917509 rev/day
Decay rate: 5.33077e-05 rev/day^2
Epoch rev: 146
Checksum: 266
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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