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N2WWD  > SAREX    21.02.97 17:38l 75 Lines 1886 Bytes #-10629 (0) @ AMSAT
BID : 13255_KC2FD
Read: GUEST OE7FMI
Subj: STS-82 Rev 127 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PHL<SP6KBL<SR6DOP<SO9ODC<SR3L<
      K3JZ<WB0TAX<KO4KS<N4HHP<N4GAA<WA2PNU<N2BQF<KC2FD
Sent: 970220/0251Z @:KC2FD.#NLI.NY.USA.NA #:13255 [Coram_LI] $:13255_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

rz
**00000000000000
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:        97050.79265393500
                        02/19/1997  19:01:25.299 UTC
EFG E:                   14405968.0000000 ft
    F:                   15166991.0000000 ft
    G:                   9247799.00000000 ft
    Edot:                -18119.689999999 ft/s
    Fdot:                13379.3500000000 ft/s
    Gdot:                6263.80000000000 ft/s
ndot/2 (drag):              0.00000195506 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        2.14271E-05 1/Earth Radii
Elset #:                               35
Rev @ Epoch:              127.16131967213
 
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   97050.79265393  .00000196  00000-0  21427-4 0   355
2 24719  28.4702  66.9247 0014177  56.3434   1.7467 14.86733716  1278
 
Satellite: STS-82      
Catalog number: 24719
Epoch time:      97050.79265393
Element set:      35
Inclination:       28.4702 deg
RA of node:        66.9247 deg
Eccentricity:    0.0014177
Arg of perigee:    56.3434 deg
Mean anomaly:       1.7467 deg
Mean motion:   14.86733716 rev/day
Decay rate:    1.95506e-06 rev/day^2
Epoch rev:             127
Checksum:              325
 
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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