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N2WWD > SAREX 26.05.96 02:41l 59 Lines 1722 Bytes #-11003 (0) @ AMSAT
BID : 32829_KC2FD
Read: GUEST OE7FMI
Subj: STS-77 Rev 94 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PHL<OK0PRG<OK0PAB<PU3DTA<F6CNB<
WB0TAX<KO4KS<N4HHP<N4GAA<N2BQF<KC2FD
Sent: 960525/0710Z @:KC2FD.#NLI.NY.USA.NA #:32829 [Coram, NY] $:32829_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 94 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: 96146.25019550900
05/25/1996 06:00:16.891 UTC
ECI X: -2748.9529515215 km
Y: -5975.3315936716 km
Z: 968.832999999999 km
Xdot: 5.82128724148925 km/s
Ydot: -1.9091579970654 km/s
Zdot: 4.74876700000000 km/s
ndot/2 (drag): 0.00005659430 rev/day^2
nddt/6: 1.33648E-10 rev/day^3
Bstar: 1.12536E-05 1/Earth Radii
Elset #: 18
Rev @ Epoch: 94.03712980598
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 96146.25019551 .00005659 13365-9 11254-4 0 185
2 23870 39.0105 234.8109 0012882 329.2984 44.0684 15.98648253 945
Satellite: STS-77
Catalog number: 23870
Epoch time: 96146.25019551
Element set: 18
Inclination: 39.0105 deg
RA of node: 234.8109 deg
Eccentricity: 0.0012882
Arg of perigee: 329.2984 deg
Mean anomaly: 44.0684 deg
Mean motion: 15.98648253 rev/day
Decay rate: 5.65943e-05 rev/day^2
Epoch rev: 94
Check sum: 331
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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