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N2WWD  > SAREX    09.04.97 10:28l 62 Lines 1856 Bytes #-10581 (0) @ AMSAT
BID : 24095_KC2FD
Read: OE5GD GUEST OE7FMI
Subj: STS-83 Rev 28 Orbital Data
Path: DB0AAB<DB0KCP<DB0ULM<DB0LX<DB0RBS<DB0SEL<DB0ZDF<DB0SRS<DB0MW<DB0AIS<
      DB0NDK<DB0ACH<ON4RAT<ON1ANR<ON6AR<F6CNB<WB0TAX<WB7AWL<KA6EYH<PY1AA<
      PY1CYL<KC6UFM<K2ADJ<WT3V<KC2PB<WB2COP<WA2SNA<WA2AWG<N2BQF<KC2FD
Sent: 970406/1349Z @:KC2FD.#NLI.NY.USA.NA #:24095 [Coram_LI] $:24095_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:        97096.50182986100
                        04/06/1997  12:02:38.099 UTC
EFG E:                   19240656.0000000 ft
    F:                   1772392.00000000 ft
    G:                   10298002.0000000 ft
    Edot:                -3206.9299999999 ft/s
    Fdot:                23673.0099999999 ft/s
    Gdot:                1930.24000000000 ft/s
ndot/2 (drag):              0.00013900340 rev/day^2
nddt/6:                       8.10730E-10 rev/day^3
Bstar:                        4.30385E-05 1/Earth Radii
Elset #:                                9
Rev @ Epoch:               28.22443718389
 
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   97096.50182986  .00013900  81073-9  43038-4 0    98
2 24755  28.4694 301.1348 0003622 342.2995  98.5036 15.90404225   288
 
Satellite: STS-83      
Catalog number: 24755
Epoch time:      97096.50182986
Element set:       9
Inclination:       28.4694 deg
RA of node:       301.1348 deg
Eccentricity:    0.0003622
Arg of perigee:   342.2995 deg
Mean anomaly:      98.5036 deg
Mean motion:   15.90404225 rev/day
Decay rate:    1.39003e-04 rev/day^2
Epoch rev:              28
Checksum:              310
 
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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