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N2WWD  > SAREX    14.07.97 12:15l 61 Lines 2028 Bytes #-10397 (0) @ AMSAT
BID : 41893_KC2FD
Read: GUEST OE7FMI
Subj: STS-94 rev 188 Orbital Data
Path: DB0RGB<DB0MAK<OK0PKL<DB0JES<DB0GR<DB0BLO<DB0TGM<DB0SAW<DB0LWL<DF0HMB<
      DB0HES<OZ7BOX<OZ2BOF<OZ9PAC<OZ5BBS<OZ4PAC<OZ4BBS<OZ3PAC<OZ6BBS<SK7CY<
      SK6FV<SK6YW<SK7YX<SK7QJ<SK7HR<SM7FEJ<SM6JZZ<SK4HC<SK5BB<SK5AE<SK5UM<
      SK0MK<SK0QO<SM0GJK<OH0RBA<OH1RBU<OH7RBA<KE4GAJ<KA0WIN<WB0TAX<KE2VW<
      KB2OBB<KC2UA<KC5ELH<N2BQF<KC2FD
Sent: 970713/1423Z @:KC2FD.#NLI.NY.USA.NA #:41893 [Coram_LI] $:41893_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

STS-94
1 24849U 97032A   97194.50359954  .00057866  14043-7  17213-3 0   492
2 24849  28.4709 293.0097 0004333 103.1683  81.7816 15.91175505  1881

Launch time for STS-94: 01 JUL 97 @ 18:02:00.063 UTC

Earth-Fixed Greenwich State Vector:

Vector format = 117
Satellite Name:         STS-94
Catalog Number:         24849  97032A
Epoch Date/Time:        97194.50359953700
                        07/13/1997  12:05:10.999 UTC
EFG E:                   21805696.0000000 ft
    F:                   1814058.00000000 ft
    G:                   -920328.00000000 ft
    Edot:                -2199.3600000000 ft/s
    Fdot:                20609.4799999999 ft/s
    Gdot:                -12054.260000000 ft/s
ndot/2 (drag):              0.00057866381 rev/day^2
nddt/6:                       1.40432E-08 rev/day^3
Bstar:                        1.72133E-04 1/Earth Radii
Elset #:                               49
Rev @ Epoch:              188.51374099136
Satellite: STS-94
Catalog number: 24849
Epoch time:      97194.50359954
Element set:      49
Inclination:       28.4709 deg
RA of node:       293.0097 deg
Eccentricity:    0.0004333
Arg of perigee:   103.1683 deg
Mean anomaly:      81.7816 deg
Mean motion:   15.91175505 rev/day
Decay rate:    5.78664e-04 rev/day^2
Epoch rev:             188
Checksum:              349

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 2.0. 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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