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N2WWD  > SAREX    27.09.97 12:29l 64 Lines 1826 Bytes #-10319 (0) @ AMSAT
BID : 53641_KC2FD
Read: GUEST OE7FMI
Subj: STS-86 Rev 1 Orbital Data
Path: DB0AAB<DB0KFB<DB0ZKA<DB0ABH<DB0SRS<DB0MW<DB0ERF<DB0SAW<DB0HRO<DB0OQ<
      DB0IL<OZ5BBS<OZ4PAC<OZ4BBS<OZ3PAC<OZ6BBS<SK7CY<SK6FV<SK6YW<SK6BA<
      SK6LK<SM7FEJ<SM6JZZ<SK4HC<SK5BB<SK5AE<SK0MK<SK0QO<SM0GJK<OH0RBA<OH1RBU<
      OH7RBA<HA3PG<PY1AA<KA6EYH<KO4KS<N4HHP<N4GAA<N2BQF<KC2FD
Sent: 970926/0436Z @:KC2FD.#NLI.NY.USA.NA #:53641 [Coram_LI] $:53641_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for
STS-86.  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-86
Catalog Number:         24964  97055A
Epoch Date/Time:        97269.13748726900
                        09/26/1997  03:17:58.900 UTC
EFG E:                   6614698.00000000 ft
    F:                   20543550.0000000 ft
    G:                   -3742877.0000000 ft
    Edot:                -14705.670000000 ft/s
    Fdot:                1191.90000000000 ft/s
    Gdot:                -19385.459999999 ft/s
ndot/2 (drag):              0.00050150800 rev/day^2
nddt/6:                       1.04870E-08 rev/day^3
Bstar:                        9.46296E-05 1/Earth Radii
Elset #:                                1
Rev @ Epoch:                1.53507853576

Launch occurred: 26-SEP-97 / 02:34:19.072 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector, using a 1.0 drag multiplier:

STS-86
1 24964U 97055A   97269.13748727  .00050151  10487-7  94630-4 0    12
2 24964  51.6548 298.7294 0031237 351.0989 201.5193 15.99060847    19

Satellite: STS-86
Catalog number: 24964
Epoch time:      97269.13748727
Element set:       1
Inclination:       51.6548 deg
RA of node:       298.7294 deg
Eccentricity:    0.0031237
Arg of perigee:   351.0989 deg
Mean anomaly:     201.5193 deg
Mean motion:   15.99060847 rev/day
Decay rate:    5.01508e-04 rev/day^2
Epoch rev:               1
Checksum:              331

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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