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N2WWD  > SAREX    08.04.97 14:59l 62 Lines 1822 Bytes #-10582 (0) @ AMSAT
BID : 23085_KC2FD
Read: GUEST OE7FMI
Subj: STS-83 Rev 1 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<DB0SON<DB0SIF<DB0AIS<DB0NDK<DB0ACH<ON4RAT<ON1ANR<
      ON6AR<F6CNB<WB0TAX<KE2VW<W2IM<KB2FAF<KA3VRW<KB3BHH<N2ERH<WA2SNA<WA2AWG<
      N2BQF<KC2FD
Sent: 970404/2259Z @:KC2FD.#NLI.NY.USA.NA #:23085 [Coram_LI] $:23085_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT


Below is the current State Vector and Keplerian Elements for STS-83.
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-83
Catalog Number:         24755  97013A
Epoch Date/Time:        97094.83532870400
                        04/04/1997  20:02:52.400 UTC
EFG E:                   11073776.0000000 ft
    F:                   16617300.0000000 ft
    G:                   -9037303.0000000 ft
    Edot:                -20663.569999998 ft/s
    Fdot:                10473.6599999998 ft/s
    Gdot:                -6055.1000000000 ft/s
ndot/2 (drag):              0.00013355263 rev/day^2
nddt/6:                       7.48556E-10 rev/day^3
Bstar:                        4.20997E-05 1/Earth Radii
Elset #:                                1
Rev @ Epoch:                1.66644315838

Launch occurred: 04-APR-97 / 19:20:32.088 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.5 drag multiplier:

STS-83
1 24755U 97013A   97094.83532870  .00013355  74856-9  42100-4 0    19
2 24755  28.4682 313.5699 0002751 326.1841 273.7513 15.90058988    13

Satellite: STS-83
Catalog number: 24755
Epoch time:      97094.83532870
Element set:       1
Inclination:       28.4682 deg
RA of node:       313.5699 deg
Eccentricity:    0.0002751
Arg of perigee:   326.1841 deg
Mean anomaly:     273.7513 deg
Mean motion:   15.90058988 rev/day
Decay rate:    1.33553e-04 rev/day^2
Epoch rev:               1
Checksum:              316

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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