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N2WWD  > SAREX    19.08.97 05:42l 109 Lines 3891 Bytes #-10359 (0) @ AMSAT
BID : 46479_KC2FD
Read: GUEST OE7FMI
Subj: STS-85 Rev 36 Orbital Data
Path: DB0RGB<DB0MAK<OK0PKL<DB0TUD<DB0NDR<DB0FHO<DK5SG<N0MPI<N0ARY<KC5ELH<
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From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
To  : SAREX@AMSAT

Below is the current State Vectors and Keplerian Elements for=20
STS-85.  The vector data comes from NASA; the Keplerian Elements=20
were computed from the vector. =20
=20
This file may be read by VEC2TLE version 9648 to update your=20
Keplerian Elements text file.
=20
Vector format =3D 117
Satellite Name:         STS-85
Catalog Number:         24889  97039A   =20
Epoch Date/Time:        97221.82920254600
                        08/09/1997  19:54:03.099 UTC
EFG E:                   12987418.0000000 ft
    F:                   -11337323.000000 ft
    G:                   13496401.0000000 ft
    Edot:                19218.0400000000 ft/s
    Fdot:                4835.14999999999 ft/s
    Gdot:                -14405.940000000 ft/s
ndot/2 (drag):              0.00031279690 rev/day^2
nddt/6:                       4.09480E-09 rev/day^3
Bstar:                        8.81047E-05 1/Earth Radii
Elset #:                                8
Rev @ Epoch:               36.36838131528
=20
Vector format =3D 117
Satellite Name:         CRISTA/SPAS
Catalog Number:         24890  97039B   =20
Epoch Date/Time:        97221.79389930600
                        08/09/1997  19:03:12.900 UTC
EFG E:                   -7754373.0000000 ft
    F:                   10936952.0000000 ft
    G:                   -17307890.000000 ft
    Edot:                -22888.290000000 ft/s
    Fdot:                -5018.2299999999 ft/s
    Gdot:                7082.71000000000 ft/s
ndot/2 (drag):              0.00031916835 rev/day^2
nddt/6:                       4.26335E-09 rev/day^3
Bstar:                        9.00638E-05 1/Earth Radii
Elset #:                                7
Rev @ Epoch:               36.80407314350
=20
Launch: 07-AUG-97 / 14:41:00.082 UTC
=20
The following Keplerian elements were computed by VEC2TLE from this
vector, using a 1.0 drag multiplier:
=20
STS-85     =20
1 24889U 97039A   97221.82920255  .00031280  40948-8  88105-4 0    87
2 24889  56.9976  66.3225 0008802 288.5734 204.0760 15.92815149   367
CRISTA/SPAS=20
1 24890U 97039B   97221.79389931  .00031917  42633-8  90064-4 0    71
2 24890  56.9978  66.4892 0007198 279.9633   9.5233 15.92804141   364
=20
Satellite: STS-85     =20
Catalog number: 24889
Epoch time:      97221.82920255
Element set:       8
Inclination:       56.9976 deg
RA of node:        66.3225 deg
Eccentricity:    0.0008802
Arg of perigee:   288.5734 deg
Mean anomaly:     204.0760 deg
Mean motion:   15.92815149 rev/day
Decay rate:    3.12797e-04 rev/day^2
Epoch rev:              36
Checksum:              337
=20
Satellite: CRISTA/SPAS=20
Catalog number: 24890
Epoch time:      97221.79389931
Element set:       7
Inclination:       56.9978 deg
RA of node:        66.4892 deg
Eccentricity:    0.0007198
Arg of perigee:   279.9633 deg
Mean anomaly:       9.5233 deg
Mean motion:   15.92804141 rev/day
Decay rate:    3.19168e-04 rev/day^2
Epoch rev:              36
Checksum:              344
=20
VEC2TLE may be downloaded from:
=20
http://www.amsat.org/amsat/sarex/orbit.html
=20
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
=20



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