HR1RBB > SAREX 28.05.96 20:59l 62 Lines 1765 Bytes #-11000 (0) @ AMSAT
BID : 17769_HR1PAQ
Read: GUEST OE7FMI
Subj: STS-77 Rev 114 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PRG<OK0PAB<PU3DTA<F6CNB<K5ARH<
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Sent: 960528/0149Z @:HR1PAQ.#TGU.HON.CEAM #:17769 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-77 Rev 114 Orbital Data
S T S - 7 7 O R B I T A L D A T A
Below is the rev 114 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: 96147.54248379630
05/26/1996 13:01:10.600 UTC
EFG E: 14004065 ft
F: 10323599 ft
G: -13223675 ft
Edot: -16637.77 ft/s
Fdot: 16939.89 ft/s
Gdot: -4373.24 ft/s
ndot/2 (drag): 0.00004911482 rev/day^2
nddt/6: 1.00778E-10 rev/day^3
Bstar: 1.09388E-05 1/Earth Radii
Elset #: 23
Rev @ Epoch: 114.70593689483
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 96147.54248380 .00004911 10078-9 10939-4 0 235
2 23870 39.0131 226.2052 0007973 303.4372 310.7003 15.96728106 1141
Satellite: STS-77
Catalog number: 23870
Epoch time: 96147.54248380
Element set: 23
Inclination: 39.0131 deg
RA of node: 226.2052 deg
Eccentricity: 0.0007973
Arg of perigee: 303.4372 deg
Mean anomaly: 310.7003 deg
Mean motion: 15.96728106 rev/day
Decay rate: 4.91148e-05 rev/day^2
Epoch rev: 114
Checksum: 285
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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