HR1RBB > SAREX 24.06.96 06:09l 63 Lines 1942 Bytes #-10972 (0) @ AMSAT
BID : 19298_HR1PAQ
Read: GUEST OE7FMI
Subj: STS-78 Rev 15 Orbital Data
Path: DB0AAB<DB0FSG<DB0SL<DB0RGB<OK0PPL<OK0PKL<OK0PPR<OK0PRG<OK0PAB<PU3DTA<
WB0TAX<K5ARH<KB5OGN<KA1XN<V31LO<HR1PAQ
Sent: 960621/2303Z @:HR1PAQ.#TGU.HON.CEAM #:19298 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-78 Rev 15 Orbital Data
S T S - 7 8 O R B I T A L D A T A
Below is the rev 15 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: 96173.50125578700
06/21/1996 12:01:48.499 UTC
EFG E: 16938215 ft
F: 779934 ft
G: 13725453 ft
Edot: -1286.34 ft/s
Fdot: 24130.97 ft/s
Gdot: 222.28 ft/s
ndot/2 (drag): 0.00013200042 rev/day^2
nddt/6: 7.26162E-10 rev/day^3
Bstar: 2.35758E-05 1/Earth Radii
Elset #: 5
Rev @ Epoch: 15.24776279058
Launch was 20-JUN-96 / 14:49:00.093
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.25 drag multiplier:
STS-78
1 23931U 96036A 96173.50125579 .00013200 72616-9 23576-4 0 54
2 23931 39.0143 4.0637 0007869 281.3346 167.8600 16.00622230 153
Satellite: STS-78
Catalog number: 23931
Epoch time: 96173.50125579
Element set: 5
Inclination: 39.0143 deg
RA of node: 4.0637 deg
Eccentricity: 0.0007869
Arg of perigee: 281.3346 deg
Mean anomaly: 167.8600 deg
Mean motion: 16.00622230 rev/day
Decay rate: 1.32000e-04 rev/day^2
Epoch rev: 15
Checksum: 265
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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