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N2WWD  > SAREX    17.02.97 11:30l 72 Lines 1856 Bytes #-10634 (0) @ AMSAT
BID : 12630_KC2FD
Read: GUEST OE7FMI
Subj: STS-82 Rev 68 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<SP6KBL<SR6DOP<SO9ODC<SR3KWX<K3JZ<
      WB0TAX<KO4KS<N4HHP<N4GAA<WA2PNU<W2NRE<WA2SNA<WA2AWG<N2BQF<KC2FD
Sent: 970215/2123Z @:KC2FD.#NLI.NY.USA.NA #:12630 [Cora630_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:        97046.83556365700
                        02/15/1997  20:03:12.699 UTC
EFG E:                   9180604.00000000 ft
    F:                   18633399.0000000 ft
    G:                   9567402.00000000 ft
    Edot:                -21353.299999999 ft/s
    Fdot:                7604.92000000000 ft/s
    Gdot:                5665.64999999999 ft/s
ndot/2 (drag):              0.00000209186 rev/day^2
nddt/6:                0.00000E+00 rev/day^3
Bstar:                        2.14824E-05 1/Earth Radii
Elset #:                               19
Rev @ Epoch:               68.17056581768
 
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   97046.83556366  .00000209  00000-0  21482-4 0   196
2 24719  28.4712  92.2355 0002770  38.0115  23.4063 14.89432063   681
 
Satellite: STS-82      
Catalog number: 24719
Epoch time:      97046.83556366
Element set:      19
Inclination:       28.4712 deg
RA of node:        92.2355 deg
Eccentricity:    0.0002770
Arg of perigee:    38.0115 deg
Mean anomaly:      23.4063 deg
Mean motion:   14.89432063 rev/day
Decay rate:    2.09186e-06 rev/day^2
Epoch rev:              68
Checksum:              303
 
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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