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N2WWD  > SAREX    23.05.97 18:28l 65 Lines 2066 Bytes #-10535 (0) @ AMSAT
BID : 33259_KC2FD
Read: DL3MFH GUEST OE7FMI
Subj: STS-84 Rev 102 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<DB0SON<DB0SIF<DB0NHM<DB0SAW<DB0HRO<OZ4BOX<OZ3BOS<
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Sent: 970522/0035Z @:KC2FD.#NLI.NY.USA.NA #:33259 [Coram_LI] $:33259_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

STS-84
1 24804U 97023A   97141.79335995  .00002735  00000-0  33799-4 0   231
2 24804  51.6525 218.4634 0007374  65.2261  41.8067 15.59433301  1028

Launch time for STS-84: 15 MAY 97 @ 08:07:48.076 UTC

Earth-Fixed Greenwich State Vector:

Vector format = 117
Satellite Name:         STS-84
Catalog Number:         24804  97023A
Epoch Date/Time:        97141.79335995400
                        05/21/1997  19:02:26.300 UTC
EFG E:                   -14447608.000000 ft
    F:                   2603520.00000000 ft
    G:                   16611486.0000000 ft
    Edot:                -10497.090000000 ft/s
    Fdot:                -21029.020000000 ft/s
    Gdot:                -5803.1099999999 ft/s
ndot/2 (drag):              0.00002735355 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        3.37990E-05 1/Earth Radii
Elset #:                               23
Rev @ Epoch:              102.29727868799

Keplerian Elements (Amsat format):

Satellite: STS-84
Catalog number: 24804
Epoch time:      97141.79335995
Element set:      23
Inclination:       51.6525 deg
RA of node:       218.4634 deg
Eccentricity:    0.0007374
Arg of perigee:    65.2261 deg
Mean anomaly:      41.8067 deg
Mean motion:   15.59433301 rev/day
Decay rate:    2.73535e-05 rev/day^2
Epoch rev:             102
Checksum:              299

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

----------
David H. Ransom, Jr.   Email:rans7500@spacelink.msfc.nasa.gov





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