HR1RBB > SAREX 01.07.96 15:17l 68 Lines 1946 Bytes #-10964 (0) @ WW
BID : 19499_HR1PAQ
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Subj: STS-78 Rev 79 Orbital Data
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Sent: 960625/1559Z @:HR1PAQ.#TGU.HON.CEAM #:19499 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-78 Rev 79 Orbital Data
S T S - 7 8 O R B I T A L D A T A
Below is the rev 79 State Vector and Keplerian Elements for STS-78.
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) 262-6782 or by telnet: oig1.gsfc.nasa.gov
(UserID = oig / Password = goddard1).
Vector format = 117
Satellite Name: STS-78
Catalog Number: 23931 96036A
Epoch Date/Time: 96177.50220601900
06/25/1996 12:03:10.600 UTC
EFG E: 16703435 ft
F: 11793648 ft
G: 7599524 ft
Edot: -7231.95 ft/s
Fdot: 18849.24 ft/s
Gdot: -13321.02 ft/s
ndot/2 (drag): 0.00056056077 rev/day^2
nddt/6: 1.30875E-08 rev/day^3
Bstar: 9.44626E-05 1/Earth Radii
Elset #: 16
Rev @ Epoch: 79.40652267579
Launch was 20-JUN-96 / 14:49:00.093
The following Keplerian elements were computed by VEC2TLE from this
vector using a 1.0 drag multiplier:
STS-78
1 23931U 96036A 96177.50220602 .00056056 13088-7 94463-4 0 168
2 23931 39.0125 337.2535 0007372 303.6405 202.7072 16.01623851 797
Satellite: STS-78
Catalog number: 23931
Epoch time: 96177.50220602
Element set: 16
Inclination: 39.0125 deg
RA of node: 337.2535 deg
Eccentricity: 0.0007372
Arg of perigee: 303.6405 deg
Mean anomaly: 202.7072 deg
Mean motion: 16.01623851 rev/day
Decay rate: 5.60561e-04 rev/day^2
Epoch rev: 79
Checksum: 275
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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