FW: STS-91 Nominal Orbital Data

Holwerda Wim W (wim.holwerda@waalwijk.zeneca.com)
Wed, 6 May 1998 08:01:53 +0100

Dear satellite observers,

As there has been a discussion lately on the Seesat list whether or not
the next shuttle would be visible (weather permitting) shortly after
launch from W. Europe, I feel it could be useful forwarding this
meesage.

Best regards,

Wim Holwerda (wim.holwerda@waalwijk.zeneca.com)
>----------
>From: 	Kenneth J. Ernandes[SMTP:n2wwd@mindspring.com]
>Sent: 	Wednesday, May 06, 1998 2:32 AM
>To: 	Multiple recipients of list
>Subject: 	STS-91 Nominal Orbital Data
>
>Below is the nominal State Vector and Keplerian Elements for 
>STS-91.  The vector data comes from NASA; the Keplerian Elements 
>were computed from the vector.  
>
>This file may be read by VEC2TLE version 9648 to update your 
>Keplerian Elements text file.
>
>Vector format = 10117
>Satellite Name:         STS-91
>Catalog Number:         99991            
>Epoch MET:                  0.03055722222
>                           0/00:44:00.144 MET
>EFG E:                          6371211.1 ft
>    F:                         20626945.3 ft
>    G:                         -4094598.0 ft
>    Edot:                   -14765.940587 ft/s
>    Fdot:                      749.245859 ft/s
>    Gdot:                   -19202.817137 ft/s
>ndot/2 (drag):              0.00019197128 rev/day^2
>nddt/6:                       1.52887E-09 rev/day^3
>Bstar:                        1.21815E-05 1/Earth Radii
>Elset #:                                1
>Rev @ Epoch:                1.53816461226
>
>Launch scheduled: 02-JUN-98 / 22:10 UTC
>
>The following Keplerian elements were computed by VEC2TLE from this
>vector, using a 0.1 drag multiplier:
>
>STS-91      
>1 99991U          98153.95416833  .00019197  15289-8  12182-4 0    14
>2 99991  51.6585 118.9054 0094758   9.4673 184.2603 16.07166530    19
>
>Satellite: STS-91      
>Catalog number: 99991
>Epoch time:      98153.95416833
>Element set:       1
>Inclination:       51.6585 deg
>RA of node:       118.9054 deg
>Eccentricity:    0.0094758
>Arg of perigee:     9.4673 deg
>Mean anomaly:     184.2603 deg
>Mean motion:   16.07166530 rev/day
>Decay rate:    1.91971e-04 rev/day^2
>Epoch rev:               1
>Checksum:              329
>
>VEC2TLE may be downloaded from the Web page listed below.
>
>Ken Ernandes
>n2wwd@amsat.org
>http://www.mindspring.com/~n2wwd
>
>
>