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N2WWD  > SAREX    07.07.97 09:54l 60 Lines 1844 Bytes #-10405 (0) @ AMSAT
BID : 39822_KC2FD
Read: GUEST OE7FMI
Subj: STS-94 Rev 61 Orbital Data
Path: DB0RGB<DB0SL<DB0FSG<DB0AAB<DB0KCP<DB0KFB<DB0ZKA<DB0ABH<DB0SRS<DB0SIF<
      DB0NHM<DB0SHG<DB0HSK<PI8DRS<PI8DAZ<PI8APD<PI8GCB<PI8WFL<PI8VNW<PE0MAR<
      VK5ASF<PP5BLU<KA6EYH<WB0TAX<KC6UFM<K2ADJ<WT3V<KC2PB<WB2COP<WA2SNA<
      WA2AWG<N2BQF<KC2FD
Sent: 970705/1320Z @:KC2FD.#NLI.NY.USA.NOAM #:39822 [Coram_LI] $:39822_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:        97186.50161689800
                        07/05/1997  12:02:19.699 UTC
EFG E:                   -11912464.000000 ft
    F:                   -18219219.000000 ft
    G:                   -2431568.0000000 ft
    Edot:                16739.3199999999 ft/s
    Fdot:                -12497.370000000 ft/s
    Gdot:                11767.2299999999 ft/s
ndot/2 (drag):              0.00055231244 rev/day^2
nddt/6:                       1.27994E-08 rev/day^3
Bstar:                        1.70880E-04 1/Earth Radii
Elset #:                               17
Rev @ Epoch:               61.96279501181

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   97186.50161690  .00055231  12799-7  17088-3 0   176
2 24849  28.4664 352.8248 0003343   7.8241 338.7739 15.90420481   617

Satellite: STS-94
Catalog number: 24849
Epoch time:      97186.50161690
Element set:      17
Inclination:       28.4664 deg
RA of node:       352.8248 deg
Eccentricity:    0.0003343
Arg of perigee:     7.8241 deg
Mean anomaly:     338.7739 deg
Mean motion:   15.90420481 rev/day
Decay rate:    5.52312e-04 rev/day^2
Epoch rev:              61
Checksum:              311

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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