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N2WWD  > SAREX    27.09.97 19:50l 60 Lines 1823 Bytes #-10319 (0) @ AMSAT
BID : 53665_KC2FD
Read: DG4MFA GUEST OE7FMI
Subj: STS-86 Rev 7 Orbital Data
Path: DB0AAB<DB0KFB<DB0CZ<DB0GE<LX0PAC<ON5VL<ON1ANR<PI8HWB<PI8ZAA<PI8GCB<
      PI8MBQ<PI8VNW<PE0MAR<OH7RBA<HA3PG<PY1AA<KA6EYH<WB0TAX<KA0WIN<KA3FMO<
      W3CH<N3ACL<WB3JOE<WA3TSW<K2ADJ<WT3V<KC2PB<WB2COP<WA2SNA<K2PUT<N2BQF<
      KC2FD
Sent: 970926/1354Z @:KC2FD.#NLI.NY.USA.NOAM #:53665 [Coram_LI] $:53665_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
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:        97269.50026388900
                        09/26/1997  12:00:22.800 UTC
EFG E:                   -9825948.0000000 ft
    F:                   -10541198.000000 ft
    G:                   16416755.0000000 ft
    Edot:                12315.7700000000 ft/s
    Fdot:                -20381.720000000 ft/s
    Gdot:                -5665.3500000000 ft/s
ndot/2 (drag):              0.00020835598 rev/day^2
nddt/6:                       1.83038E-09 rev/day^3
Bstar:                        8.96530E-05 1/Earth Radii
Elset #:                                4
Rev @ Epoch:                7.29555101521

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   97269.50026389  .00020836  18304-8  89653-4 0    42
2 24964  51.6538 296.8387 0060412  96.2396  10.1711 15.81357090    73

atellite: STS-86
Catalog number: 24964
Epoch time:      97269.50026389
Element set:       4
Inclination:       51.6538 deg
RA of node:       296.8387 deg
Eccentricity:    0.0060412
Arg of perigee:    96.2396 deg
Mean anomaly:      10.1711 deg
Mean motion:   15.81357090 rev/day
Decay rate:    2.08356e-04 rev/day^2
Epoch rev:               7
Checksum:              317

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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