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N2WWD  > SAREX    18.02.97 19:20l 59 Lines 1818 Bytes #-10633 (0) @ AMSAT
BID : 12629_KC2FD
Read: GUEST OE7FMI
Subj: STS-82 Rev 63 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<DB0SON<DB0SIF<DB0GV<DB0ZDF<DB0SEL<DB0KLN<DB0HOM<
      F6KDL<F6KFG<F6KWP<F6KIF<F5KGR<F1NWC<F1HPZ<ON4MOU<KC5ELH<N2BQF<KC2FD
Sent: 970215/1406Z @:KC2FD.#NLI.NY.USA.NA #:12629 [Coram_LI] $:12629_KC2FD
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:        97046.54383217600
                        02/15/1997  13:03:07.100 UTC
EFG E:                   13376122.0000000 ft
    F:                   15674327.0000000 ft
    G:                   -9970545.0000000 ft
    Edot:               -15777.170000000 ft/s
    Fdot:                16509.7799999999 ft/s
    Gdot:                4796.80000000000 ft/s
ndot/2 (drag):              0.00000210713 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        2.12956E-05 1/Earth Radii
Elset #:                               18
Rev @ Epoch:               63.81654090623

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   97046.54383218  .00000211  00000-0  21296-4 0   183
2 24719  28.4711  94.1104 0000775 100.6970 193.2453 14.90076050   637

Satellite: STS-82
Catalog number: 24719
Epoch time:      97046.54383218
Element set:      18
Inclination:       28.4711 deg
RA of node:        94.1104 deg
Eccentricity:    0.0000775
Arg of perigee:   100.6970 deg
Mean anomaly:     193.2453 deg
Mean motion:   14.90076050 rev/day
Decay rate:    2.10713e-06 rev/day^2
Epoch rev:              63
Checksum:              278

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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