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N2WWD > SAREX 26.05.96 03:49l 64 Lines 1729 Bytes #-11003 (0) @ AMSAT
BID : 32830_KC2FD
Read: GUEST OE7FMI
Subj: STS-77 Rev 98 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PRG<OK0PAB<OK0PBB<OK0PKR<OM0PBB<
HA5KDF<HG8GL<HA5OB<WX3K<WB7AWL<WB0TAX<KO4KS<N4HHP<N4GAA<N2BQF<KC2FD
Sent: 960525/0809Z @:KC2FD.#NLI.NY.USA.NA #:32830 [Coram, NY] $:32830_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 98 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: 96146.50126620370
05/25/1996 12:01:49.399 UTC
EFG E: -21283953.0 ft
F: -1739222.0 ft
G: 4573465.0 ft
Edot: 4740.44 ft/s
Fdot: -18300.83 ft/s
Gdot: 15087.98 ft/s
ndot/2 (drag): 0.00005037792 rev/day^2
nddt/6: 1.05998E-10 rev/day^3
Bstar: 1.09462E-05 1/Earth Radii
Elset #: 19
Rev @ Epoch: 98.05398940366
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 96146.50126620 .00005038 10600-9 10946-4 0 197
2 23870 39.0143 233.1377 0007102 306.6959 72.7406 15.97186442 986
Satellite: STS-77
Catalog number: 23870
Epoch time: 96146.50126620
Element set: 19
Inclination: 39.0143 deg
RA of node: 233.1377 deg
Eccentricity: 0.0007102
Arg of perigee: 306.6959 deg
Mean anomaly: 72.7406 deg
Mean motion: 15.97186442 rev/day
Decay rate: 5.03779e-05 rev/day^2
Epoch rev: 98
Checksum: 316
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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