HR1RBB > SAREX 29.05.96 00:35l 58 Lines 1721 Bytes #-10999 (0) @ AMSAT
BID : 17775_HR1PAQ
Read: GUEST OE7FMI
Subj: STS-77 Rev 130 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PRG<OK0PAB<PU3DTA<F6CNB<K5ARH<
KB5OGN<KA1XN<V31LO<HR1PAQ
Sent: 960528/0209Z @:HR1PAQ.#TGU.HON.CEAM #:17775 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
S T S - 7 7 O R B I T A L D A T A
Below is the rev 130 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: 96148.50140625000
05/27/1996 12:02:01.500 UTC
EFG E: -20959150 ft
F: 4444652 ft
G: 4209072 ft
Edot: -915.73 ft/s
Fdot: -18772.55 ft/s
Gdot: 15233.28 ft/s
ndot/2 (drag): 0.00005088815 rev/day^2
nddt/6: 1.08148E-10 rev/day^3
Bstar: 1.09951E-05 1/Earth Radii
Elset #: 26
Rev @ Epoch: 130.04958547218
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 96148.50140625 .00005089 10815-9 10995-4 0 266
2 23870 39.0147 219.8112 0006809 322.6788 55.1722 15.97291430 1306
Satellite: STS-77
Catalog number: 23870
Epoch time: 96148.50140625
Element set: 26
Inclination: 39.0147 deg
RA of node: 219.8112 deg
Eccentricity: 0.0006809
Arg of perigee: 322.6788 deg
Mean anomaly: 55.1722 deg
Mean motion: 15.97291430 rev/day
Decay rate: 5.08882e-05 rev/day^2
Epoch rev: 130
Checksum: 307
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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