HR1RBB > SAREX 24.06.96 02:55l 64 Lines 1927 Bytes #-10973 (0) @ AMSAT
BID : 19267_HR1PAQ
Read: GUEST OE7FMI
Subj: STS-78 Rev 1 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PRG<OK0PAB<PU3DTA<WB0TAX<K5ARH<
KB5OGN<KA1XN<V31LO<HR1PAQ
Sent: 960620/2339Z @:HR1PAQ.#TGU.HON.CEAM #:19267 [Tegucigalpa] FBB5.15c
From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-78 Rev 1 Orbital Data
S T S - 7 8 O R B I T A L D A T A
Below is the rev 1 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: 96172.64756828700
06/20/1996 15:32:29.899 UTC
EFG E: 8330141 ft
F: 19408406 ft
G: -5634774 ft
Edot: -18868.85 ft/s
Fdot: 3861.05 ft/s
Gdot: -14577.77 ft/s
ndot/2 (drag): 0.00011106815 rev/day^2
nddt/6: 5.14840E-10 rev/day^3
Bstar: 2.25262E-05 1/Earth Radii
Elset #: 1
Rev @ Epoch: 1.56718172124
Launch was 20-JUN-96
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.25 drag multiplier:
STS-78
1 23931U 96036A 96172.64756829 .00011107 51484-9 22526-4 0 10
2 23931 39.0144 9.7755 0009705 339.7238 224.4618 15.98371785 12
Satellite: STS-78
Catalog number: 23931
Epoch time: 96172.64756829
Element set: 1
Inclination: 39.0144 deg
RA of node: 9.7755 deg
Eccentricity: 0.0009705
Arg of perigee: 339.7238 deg
Mean anomaly: 224.4618 deg
Mean motion: 15.98371785 rev/day
Decay rate: 1.11068e-04 rev/day^2
Epoch rev: 1
Checksum: 323
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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