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N2WWD > SAREX 29.09.97 12:31l 64 Lines 1827 Bytes #-10317 (0) @ AMSAT
BID : N6IYA15520
Read: GUEST OE7FMI
Subj: STS-86 Rev 7 Orbital Data
Path: DB0AAB<DB0KFB<DB0ZKA<DB0LX<DB0RBS<DB0SEL<DB0ZDF<DB0GE<LX0PAC<ON7RC<
ON1BWP<ON6AR<F6CNB<PP5BLU<WB0TAX<WU3V<N1UAN<N8ZFM<KC6UFM<VE7ASS<VE7VBS<
VE7DIE<N7MGZ<N7WE<KB7CNN<N7QDN<W0RLI<N6IYA<W0RLI<KC7KVT<WA7SJN<N7QDN<
KB7CNN<N7WE<VE7DIE<VE7SRY<VE7KIT<KA6EYH<WB0TAX<KA0WIN<KA3FMO<W3CH<
N3ACL<WB3JOE<WA3TSW<K2ADJ<WT3V<KC2PB<WB2COP<WA2SNA<K2PUT<N2BQF<KC2FD
Sent: 970926/1354 @:KC2FD.#NLI.NY.USA.NOAM #:53665 $: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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