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N2WWD  > SAREX    08.04.97 18:33l 65 Lines 2268 Bytes #-10581 (0) @ AMSAT
BID : 24470_KC2FD
Read: GUEST OE7FMI
Subj: STS-83 Rev 35 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<DB0SON<DB0SIF<DB0GV<DB0GE<LX0PAC<ON7RC<ON5VL<
      ON1ANR<ON6AR<F6CNB<WB0TAX<KE2VW<KB2TXP<WB2WXQ<KA3VRW<KB3BHH<N2ERH<
      WA2SNA<KB2VLX<N2BQF<KC2FD
Sent: 970407/0149Z @:KC2FD.#NLI.NY.USA.NA #:24470 [Coram_LI] $:24470_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

STS-83
1 24755U 97013A   97096.95931134  .00013741  79213-9  42252-4 0   109
2 24755  28.4682 297.7138 0003750 355.6688 190.1403 15.90537040   358

Launch time for STS-83: 04 APR 97 @ 19:20:32.088 UTC

Earth-Fixed Greenwich State Vector:

Vector format = 117
Satellite Name:         STS-83
Catalog Number:         24755  97013A
Epoch Date/Time:        97096.95931134300
                        04/06/1997  23:01:24.500 UTC
EFG E:                   11682303.0000000 ft
    F:                   -18511886.000000 ft
    G:                   -1066460.0000000 ft
    Edot:                17211.3400000000 ft/s
    Fdot:                11541.3500000000 ft/s
    Gdot:                -12029.719999999 ft/s
ndot/2 (drag):              0.00013740514 rev/day^2
nddt/6:                       7.92127E-10 rev/day^3
Bstar:                        4.22523E-05 1/Earth Radii
Elset #:                               10
Rev @ Epoch:               35.51612632521

Keplerian Elements (Amsat format):

Satellite: STS-83
Catalog number: 24755
Epoch time:      97096.95931134
Element set:      10
Inclination:       28.4682 deg
RA of node:       297.7138 deg
Eccentricity:    0.0003750
Arg of perigee:   355.6688 deg
Mean anomaly:     190.1403 deg
Mean motion:   15.90537040 rev/day
Decay rate:    1.37405e-04 rev/day^2
Epoch rev:              35
Checksum:              312

SPACE SHUTTLE ORBITAL DATA:

These 2-line elements have been generated using Ken Ernandes' program
VEC2TLE using real time state vector data supplied by DOD C-Band Radar
Network courtesy Dave Simonson. Note that the epoch of the 2-line
elements is the same as the state vector time.

Drag and B-Star parameters are internally calculated by VEC2TLE using
a drag factor of 0.5. Rev numbers use NASA orbit numbering convention.

                                   Dave Ransom
                                   RPV Astronomy BBS
                                   http://www.dransom.com
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