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N2WWD  > SAREX    18.05.97 20:52l 61 Lines 1843 Bytes #-10540 (0) @ AMSAT
BID : 32293_KC2FD
Read: GUEST OE7FMI
Subj: STS-84 Rev 24 Orbital Data
Path: DB0AAB<DB0FSG<DB0SL<DB0RGB<OK0PPL<OK0PKL<DB0JES<DB0NHM<DB0SIF<DB0SRS<
      DB0MW<DB0ERF<DB0EAM<DK0MWX<ON5VL<ON1ANR<ON6AR<F6CNB<WB0TAX<PU3DTA<
      N2MEG<KB2VLX<WA2SNA<WA2AWG<N2BQF<KC2FD
Sent: 970516/2347Z @:KC2FD.#NLI.NY.USA.NA #:32293 [Coram_LI] $:32293_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for
STS-84.  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-84
Catalog Number:         24804  97023A
Epoch Date/Time:        97136.79174421300
                        05/16/1997  19:00:06.700 UTC
EFG E:                   -13089045.000000 ft
    F:                   4843415.00000000 ft
    G:                   17079895.0000000 ft
    Edot:                -4796.2700000000 ft/s
    Fdot:                -23534.470000000 ft/s
    Gdot:                3266.00000000000 ft/s
ndot/2 (drag):              0.00010251390 rev/day^2
nddt/6:                       4.44062E-10 rev/day^3
Bstar:                        4.52609E-05 1/Earth Radii
Elset #:                                6
Rev @ Epoch:               24.22230352270

Launch: 15-MAY-97 / 08:07:48.076 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector and the scheduled launch time using a 0.5 drag multiplier:

STS-84
1 24804U 97023A   97136.79174421  .00010251  44406-9  45261-4 0    67
2 24804  51.6546 243.6012 0087594 335.3174 104.7041 15.77902459   246

Satellite: STS-84
Catalog number: 24804
Epoch time:      97136.79174421
Element set:       6
Inclination:       51.6546 deg
RA of node:       243.6012 deg
Eccentricity:    0.0087594
Arg of perigee:   335.3174 deg
Mean anomaly:     104.7041 deg
Mean motion:   15.77902459 rev/day
Decay rate:    1.02514e-04 rev/day^2
Epoch rev:              24
Checksum:              294

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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