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N2WWD > SAREX 29.05.96 00:32l 60 Lines 1710 Bytes #-11000 (0) @ AMSAT
BID : 32985_KC2FD
Read: GUEST OE7FMI
Subj: STS-77 Rev 118 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PRG<OK0PAB<PU3DTA<F6CNB<K5ARH<
KB5OGN<KA1XN<W1EDH<W1NRG<N4GAA<WA2PNU<N2BQF<KC2FD
Sent: 960526/1827Z @:KC2FD.#NLI.NY.USA.NA #:32985 [Coram, NY] $:32985_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To : SAREX@AMSAT
S T S - 7 7 O R B I T A L D A T A
Below is the rev 118 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: 96147.79259606481
05/26/1996 19:01:20.299 UTC
EFG E: 9951450 ft
F: -14245095 ft
G: -13247254 ft
Edot: 17418.68 ft/s
Fdot: 16160.63 ft/s
Gdot: -4261.16 ft/s
ndot/2 (drag): 0.00005357073 rev/day^2
nddt/6: 1.19803E-10 rev/day^3
Bstar: 1.11482E-05 1/Earth Radii
Elset #: 24
Rev @ Epoch: 118.70712656193
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 96147.79259606 .00005357 11980-9 11148-4 0 247
2 23870 39.0101 224.5406 0008553 335.5370 279.0287 15.97936038 1182
Satellite: STS-77
Catalog number: 23870
Epoch time: 96147.79259606
Element set: 24
Inclination: 39.0101 deg
RA of node: 224.5406 deg
Eccentricity: 0.0008553
Arg of perigee: 335.5370 deg
Mean anomaly: 279.0287 deg
Mean motion: 15.97936038 rev/day
Decay rate: 5.35707e-05 rev/day^2
Epoch rev: 118
Checksum: 327
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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