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N2WWD > SAREX 25.05.96 11:06l 60 Lines 1723 Bytes #-11003 (0) @ AMSAT
BID : 32593_KC2FD
Read: GUEST OE7FMI
Subj: STS-77 Rev 78 Orbital Data
Path: DB0AAB<DB0MWS<DB0RBS<DB0SEL<DB0ZDF<DB0SRS<DB0SIF<DB0NHM<DB0EAM<DB0GV<
DB0GE<LX0PAC<ON7RC<ON1BWP<ON6AR<F6CNB<WB0TAX<KO4KS<N4HHP<N4GAA<N2BQF<
KC2FD
Sent: 960524/0606Z @:KC2FD.#NLI.NY.USA.NA #:32593 [Coram, NY] $:32593_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 78 Earth-Centered Inertial (ECI) state vector for
STS-77. This vector data comes from NASA GSFC OIG RAID RBBS.
Vector format = 7
Satellite Name: STS-77
Catalog Number: 23870 96032A
Epoch Date/Time: 96145.25124004600
05/24/1996 06:01:47.139 UTC
ECI X: -1388.4452978617 km
Y: -6343.8333841215 km
Z: 1465.51500000000 km
Xdot: 6.24419704152222 km/s
Ydot: -0.3121867969549 km/s
Zdot: 4.56801800000000 km/s
ndot/2 (drag): 0.00005014275 rev/day^2
nddt/6: 1.05015E-10 rev/day^3
Bstar: 1.09206E-05 1/Earth Radii
Elset #: 15
Rev @ Epoch: 78.05681032477
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 96145.25124005 .00005014 10502-9 10921-4 0 157
2 23870 39.0097 241.4664 0008998 297.8735 82.5785 15.97114208 780
Satellite: STS-77
Catalog number: 23870
Epoch time: 96145.25124005
Element set: 15
Inclination: 39.0097 deg
RA of node: 241.4664 deg
Eccentricity: 0.0008998
Arg of perigee: 297.8735 deg
Mean anomaly: 82.5785 deg
Mean motion: 15.97114208 rev/day
Decay rate: 5.01428e-05 rev/day^2
Epoch rev: 78
Check sum: 331
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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