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N2WWD  > SAREX    02.12.96 04:59l 58 Lines 1839 Bytes #-10720 (0) @ AMSAT
BID : 1651_KC2FD
Read: GUEST OE7FMI
Subj: STS-80 Rev 169 Orbital Data
Path: DB0AAB<DB0FSG<DB0IGL<DB0KCP<DB0KFB<DB0CZ<DB0GV<DB0GE<LX0PAC<ON5VL<
      ON1ANR<ON6AR<F6CNB<WB0TAX<PU3DTA<N2MEG<KB2VLX<WA2SNA<WA2AWG<N2BQF<
      KC2FD
Sent: 961130/1030Z @:KC2FD.#NLI.NY.USA.NA #:1651 [Coram, NY] $:1651_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for STS-80.
The vector data comes from NASA; the orbital parameters were computed
from the vector.  Hourly vector updates are available from NASA GSFC
OIG RAID RBBS at (301) 262-6784 or by telnet: oig1.gsfc.nasa.gov
(UserID = oig / Password = goddard1).

Vector format = 117
Satellite Name:         STS-80
Catalog Number:         24660  96065A
Epoch Date/Time:        96335.50026041700
                        11/30/1996  12:00:22.500 UTC
EFG E:                           17505581 ft
    F:                           -9030663 ft
    G:                            9931129 ft
    Edot:                        12542.51 ft/s
    Fdot:                        19920.55 ft/s
    Gdot:                        -3928.24 ft/s
ndot/2 (drag):              0.00000512272 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        3.70367E-06 1/Earth Radii
Elset #:                               36
Rev @ Epoch:              169.30269114835

Launch was 19-NOV-96 / 19:55:47.060 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.05 drag multiplier:

STS-80
1 24660U 96065A   96335.50026042  .00000512  00000-0  37037-5 0   364
2 24660  28.4665 110.9630 0009535  29.5821  79.3755 15.72200430  1696

Satellite: STS-80
Catalog number: 24660
Epoch time:      96335.50026042
Element set:      36
Inclination:       28.4665 deg
RA of node:       110.9630 deg
Eccentricity:    0.0009535
Arg of perigee:    29.5821 deg
Mean anomaly:      79.3755 deg
Mean motion:   15.72200430 rev/day
Decay rate:    5.12272e-06 rev/day^2
Epoch rev:             169
Checksum:              285

VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util

Ken Ernandes
n2wwd@amsat.org




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