HR1RBB > SAREX 01.07.96 15:15l 67 Lines 1946 Bytes #-10964 (0) @ WW
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Subj: STS-78 Rev 67 Orbital Data
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From: HR1RBB@HR1PAQ.#TGU.HON.CEAM
To : SAREX@AMSAT
Subject: STS-78 Rev 67 Orbital Data
S T S - 7 8 O R B I T A L D A T A
Below is the rev 67 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: 96176.75203356482
06/24/1996 18:02:55.700 UTC
EFG E: 9771394 ft
F: -16869114 ft
G: 9784045 ft
Edot: 20712.39 ft/s
Fdot: 5474.57 ft/s
Gdot: -11217.76 ft/s
ndot/2 (drag): 0.00013996803 rev/day^2
nddt/6: 8.16003E-10 rev/day^3
Bstar: 2.37010E-05 1/Earth Radii
Elset #: 15
Rev @ Epoch: 67.37361629105
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 96176.75203356 .00013997 81600-9 23701-4 0 151
2 23931 39.0168 342.2858 0007440 300.2609 194.2405 16.01540739 678
Satellite: STS-78
Catalog number: 23931
Epoch time: 96176.75203356
Element set: 15
Inclination: 39.0168 deg
RA of node: 342.2858 deg
Eccentricity: 0.0007440
Arg of perigee: 300.2609 deg
Mean anomaly: 194.2405 deg
Mean motion: 16.01540739 rev/day
Decay rate: 1.39968e-04 rev/day^2
Epoch rev: 67
Checksum: 311
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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