N2WWD > SAREX 21.02.97 11:36l 70 Lines 1897 Bytes #-10630 (0) @ AMSAT
BID : 13149_KC2FD
Read: GUEST OE7FMI
Subj: STS-82 Rev 112 Orbital Data
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OK0PKL<OK0PPR<OK0PHL<SP6KBL<SR3DLE<SP3FKM<SR3BBS<SR3KWX<K3JZ<WB0TAX<
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From: N2WWD@KC2FD.#NLI.NY.USA.NA
To : SAREX@AMSAT
Below is the current State Vector and Keplerian Elements for STS-82.
The vector data comes from NASA; the Keplerian Elements were
computed from the vector.
This file may be read by VEC2TLE version 9648 to update your
Keplerian Elements text file.
Vector format = 117
Satellite Name: STS-82
Catalog Number: 24719 97004A
Epoch Date/Time: 97049.83345254600
02/18/1997 20:00:10.299 UTC
EFG E: 11588894.0000000 ft
F: -18190062.000000 ft
G: -7773724.0000000 ft
Edot: 19792.6300000000 ft/s
Fdot: 9108.36000000000 ft/s
Gdot: 8319.84000000000 ft/s
ndot/2 (drag): 0.00000191556 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 2.11742E-05 1/Earth Radii
Elset #: 31
Rev @ Epoch: 112.87461026440
Launch occurred: 11-FEB-97 / 08:55:17.087 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.5 drag multiplier:
STS-82
1 24719U 97004A 97049.83345255 .00000192 00000-0 21174-4 0 315
2 24719 28.4714 73.0477 0014751 45.0896 269.7534 14.86380588 1120
Satellite: STS-82
Catalog number: 24719
Epoch time: 97049.83345255
Element set: 31
Inclination: 28.4714 deg
RA of node: 73.0477 deg
Eccentricity: 0.0014751
Arg of perigee: 45.0896 deg
Mean anomaly: 269.7534 deg
Mean motion: 14.86380588 rev/day
Decay rate: 1.91556e-06 rev/day^2
Epoch rev: 112
Checksum: 333
VEC2TLE may be downloaded from:
http://www.amsat.org/amsat/sarex/orbit.html
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
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