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N2WWD  > SAREX    14.02.97 19:59l 65 Lines 1825 Bytes #-10637 (0) @ AMSAT
BID : 11522_KC2FD
Read: DG2MJR GUEST OE7FMI
Subj: STS-82 Tev 23 Orbital Data
Path: DB0AAB<DB0MWS<DB0ZKA<DB0LX<DB0RBS<DB0SEL<DB0ZDF<DB0AIS<DB0SIF<DB0SON<
      DB0MAK<OK0PKL<OK0PPR<OK0PHL<OK0PRG<OK0PAB<OH3RBR<PU3DTA<WB0TAX<KO4KS<
      N4HHP<N4GAA<WA2PNU<W2NRE<WA2SNA<WA2AWG<N2BQF<KC2FD
Sent: 970213/0146Z @:KC2FD.#NLI.NY.USA.NA #:11522 [Coram_LI] $:11522_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT


Below is the current State Vector and Keplerian Elements for STS-82.
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 = 117
Satellite Name:         STS-82
Catalog Number:         24719  97004A
Epoch Date/Time:        97043.83624884300
                         2/12/1997  20:04:11.900 UTC
EFG E:                    19417467.000000 ft
    F:                    130568.00000000 ft
    @:                    775558.00000000 ft
    Edot:                -11237.989999999 ft/s
    Fdot:                -19305.439999999 ft/s
    Gdot:                 6996.2299999999 ft/s
ndot/2 (drag):              0.00000249181 rev/day^2
nddt/6:                        .00000E+00 rev/day^3
Bstar:                        2.21872E-05 1/Earth Radii
Elset #:                                 
Rev @ Epoch:                3.35054353711

Launch occurred: 11-FEB-97 / 08:55:17.087 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.5 drag multiplier:

STS-82
1 24719U 97004A   97043.83624884  .00000249  00000-0  22187-4 0    89
2 24719  28.4695 111.5236 0008502 176.9859 309.1937 14.95054003   236

Satellite: STS-82
Catalog number: 24719
Epoch time:      97043.83624884
Element set:       8
Inclination:       28.4695 deg
RA of node:       111.5236 deg
Eccentricity:    0.0008502
Arg of perigee:   176.9859 deg
Mean anomaly:     309.1937 deg
Mean motion:   14.95054003 rev/day
Decay rate:    2.49181e-06 rev/day^2
Epoch rev:              23
Checksum:              323

VEC2TLE may be downloaded from:

http://www.amsat.org/amsat/sarex/orbit.html

Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd






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