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N2WWD  > SAREX    13.07.97 20:59l 64 Lines 1879 Bytes #-10398 (0) @ AMSAT
BID : 41345_KC2FD
Read: GUEST OE7FMI
Subj: STS-94 Rev 145 Orbital Data
Path: DB0RGB<DB0SL<OE3XBS<OM0PBB<HA5KDF<HG8GL<HA5OB<HA3PG<OH7RBA<VK3ECV<
      N1KIO<WU3V<WB0TAX<KE3SU<W3CH<N3ACL<WA3MQY<N2QAE<N2ERH<WA2SNA<WA2PNU<
      N2BQF<KC2FD
Sent: 970711/0000Z @:KC2FD.#NLI.NY.USA.NOAM #:41345 [Coram_LI] $:41345_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for 
STS-94.  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-94
Catalog Number:         24849  97032A    
Epoch Date/Time:        97191.79435879600
                        07/10/1997  19:03:52.599 UTC
EFG E:                   -15934281.000000 ft
    F:                   -11630079.000000 ft
    G:                   9476473.00000000 ft
    Edot:                11776.3500000000 ft/s
    Fdot:                -20272.400000000 ft/s
    Gdot:                -5041.4700000000 ft/s
ndot/2 (drag):              0.00057103082 rev/day^2
nddt/6:                       1.36792E-08 rev/day^3
Bstar:                        1.74008E-04 1/Earth Radii

Elset #:                               38
Rev @ Epoch:              145.31833238155
 
Launch: 01-JUL-97 / 18:02:00.063 UTC
 
The following Keplerian elements were computed by VEC2TLE from this
vector and the scheduled launch time using a 2.0 drag multiplier:
 
STS-94      
1 24849U 97032A   97191.79435880  .00057103  13679-7  17401-3 0   388
2 24849  28.4689 313.2762 0004546  70.3271  44.2587 15.90707223  1455
 
Satellite: STS-94      
Catalog number: 24849
Epoch time:      97191.79435880
Element set:      38
Inclination:       28.4689 deg
RA of node:       313.2762 deg
Eccentricity:    0.0004546
Arg of perigee:    70.3271 deg
Mean anomaly:      44.2587 deg
Mean motion:   15.90707223 rev/day
Decay rate:    5.71031e-04 rev/day^2
Epoch rev:             145
Checksum:              323
 
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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