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N2WWD > SAREX 07.12.96 00:30l 80 Lines 2798 Bytes #-10715 (0) @ AMSAT
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Subj: STS-80 Rev 236 Orbital Data
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Date: Wed, 4 Dec 1996 15:38:55 -0600
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From: Ken Ernandes <kene@fairchild.lmco.com>
To: Multiple recipients of list <ststle@spacelink.msfc.nasa.gov>
Subject: STS-80 Rev 236 Orbital Data
X-Listprocessor-Version: 6.0c -- ListProcessor by Anastasios Kotsikonas
X-Comment: STS Two Line Elements
X-Mailer: Windows Eudora Pro Version 2.2 (16)
Below is the current State Vector and Keplerian Elements for STS-80.
The vector data comes from NASA; the orbital parameters were computed
from the vector. Hourly vector updates are available from NASA GSFC
OIG RAID RBBS at (301) 262-6784 or by telnet: oig1.gsfc.nasa.gov
(UserID = oig / Password = goddard1).
Vector format = 117
Satellite Name: STS-80
Catalog Number: 24660 96065A
Epoch Date/Time: 96339.83586689800
12/04/1996 20:03:38.899 UTC
EFG E: 3574167 ft
F: -20835673 ft
G: -6591053 ft
Edot: 20864.30 ft/s
Fdot: 6504.71 ft/s
Gdot: -9397.36 ft/s
ndot/2 (drag): 0.00000450390 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 3.60813E-06 1/Earth Radii
Elset #: 52
Rev @ Epoch: 236.60676504408
Launch was 19-NOV-96 / 19:55:47.060 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.05 drag multiplier:
STS-80
1 24660U 96065A 96339.83586690 .00000450 00000-0 36081-5 0 521
2 24660 28.4670 79.4250 0021619 80.8154 137.6374 15.69503455 2364
Satellite: STS-80
Catalog number: 24660
Epoch time: 96339.83586690
Element set: 52
Inclination: 28.4670 deg
RA of node: 79.4250 deg
Eccentricity: 0.0021619
Arg of perigee: 80.8154 deg
Mean anomaly: 137.6374 deg
Mean motion: 15.69503455 rev/day
Decay rate: 4.50390e-06 rev/day^2
Epoch rev: 236
Checksum: 323
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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