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N2WWD > SAREX 26.05.96 11:24l 60 Lines 1709 Bytes #-11002 (0) @ AMSAT
BID : 32876_KC2FD
Read: GUEST OE7FMI
Subj: STS-77 Rev 102 Orbital Data
Path: DB0AAB<DB0KCP<DB0CZ<DB0LX<DB0RBS<DB0SEL<DB0ZDF<DB0SRS<DB0SIF<DB0SON<
DB0MAK<DB0HOT<DB0ZWI<OK0PKL<OK0PPR<OK0PRG<OK0PAB<PU3DTA<WB0TAX<KO4KS<
N4HHP<N4GAA<N2BQF<KC2FD
Sent: 960525/1543Z @:KC2FD.#NLI.NY.USA.NA #:32876 [Coram, NY] $:32876_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 102 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: 96146.79403587963
05/25/1996 19:03:24.700 UTC
EFG E: 14010653 ft
F: -9668635 ft
G: -13696870 ft
Edot: 12763.09 ft/s
Fdot: 20450.61 ft/s
Gdot: -1360.75 ft/s
ndot/2 (drag): 0.00004963390 rev/day^2
nddt/6: 1.02911E-10 rev/day^3
Bstar: 1.09697E-05 1/Earth Radii
Elset #: 21
Rev @ Epoch: 102.73650144944
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 96146.79403588 .00004963 10291-9 10970-4 0 211
2 23870 39.0115 231.1906 0008343 303.4680 321.6726 15.96860995 1023
Satellite: STS-77
Catalog number: 23870
Epoch time: 96146.79403588
Element set: 21
Inclination: 39.0115 deg
RA of node: 231.1906 deg
Eccentricity: 0.0008343
Arg of perigee: 303.4680 deg
Mean anomaly: 321.6726 deg
Mean motion: 15.96860995 rev/day
Decay rate: 4.96339e-05 rev/day^2
Epoch rev: 102
Checksum: 321
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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