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N2WWD  > SAREX    12.02.97 22:17l 62 Lines 1855 Bytes #-10641 (0) @ AMSAT
BID : 11365_KC2FD
Read: GUEST OE7FMI
Subj: STS-82 REV 7 ORBITAL DATA
Path: DB0AAB<DB0FSG<DB0IGL<DB0KCP<DB0ULM<DB0LX<DB0RBS<DB0SAO<DK5SG<N0MPI<
      N0ARY<W2XO<KA3JSD<K8LG<W3OC<WA3IOU<N8YIB<N2BQF<KC2FD
Sent: 970211/2357Z @:KC2FD.#NLI.NY.USA.NA #:11365 [Coram_LI] $:11365_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:        97042.79341435200
                        02/11/1997  19:02:31.000 UTC
EFG E:                   -1977283.0000000 ft
    F:                   -21755417.000000 ft
    G:                   -6604160.0000000 ft
    Edot:                21308.2200000000 ft/s
    Fdot:                866.600000000000 ft/s
    Gdot:                -9392.8299999999 ft/s
ndot/2 (drag):              0.00000487717 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        2.57815E-05 1/Earth Radii
Elset #:                                3
Rev @ Epoch:                7.60322584261
 
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   97042.79341435  .00000488  00000-0  25781-4 0    34
2 24719  28.4683 118.4011 0071540  49.7595 167.4178 15.12206247    79
 
Satellite: STS-82      
Catalog number: 24719
Epoch time:      97042.79341435
Element set:       3
Inclination:       28.4683 deg
RA of node:       118.4011 deg
Eccentricity:    0.0071540
Arg of perigee:    49.7595 deg
Mean anomaly:     167.4178 deg
Mean motion:   15.12206247 rev/day
Decay rate:    4.87717e-06 rev/day^2
Epoch rev:               7
Checksum:              312
 
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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