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N2WWD  > SAREX    05.10.97 07:22l 59 Lines 1851 Bytes #-10311 (0) @ AMSAT
BID : 54936_KC2FD
Read: GUEST OE7FMI
Subj: STS-86 Rev 123 Orbital Data
Path: DB0AAB<DB0FSG<DB0SL<OE3XBS<OM0PBB<HA5KDF<HG8GL<HA5OB<HA3PG<PY1AA<
      KA6EYH<WB0TAX<KA0WIN<KA3FMO<W3CH<N3ACL<WB3JOE<WA3TSW<K2ADJ<WT3V<KC2PB<
      WB2COP<WA2SNA<WA2PNU<N2BQF<KC2FD
Sent: 971004/0250Z @:KC2FD.#NLI.NY.USA.NOAM #:54936 [Coram_LI] $:54936_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 = 7
Satellite Name:         STS-86
Catalog Number:         24964  97055A    
Epoch Date/Time:        97276.96056061300
                        10/03/1997  23:03:12.436 UTC
ECI X:                   -3107.3456701607 km
    Y:                   -5394.3585342520 km
    Z:                   -2579.1419999998 km
    Xdot:                3.39336260030613 km/s
    Ydot:                -4.4628793153381 km/s
    Zdot:                5.27407799999999 km/s
ndot/2 (drag):              0.00007808040 rev/day^2
nddt/6:                       2.59401E-10 rev/day^3
Bstar:                        7.11271E-05 1/Earth Radii
Elset #:                               35
Rev @ Epoch:              123.91931482499
 
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   97276.96056061  .00007808  25940-9  71127-4 0   350
2 24964  51.6525 259.2033 0017684   1.2230 329.7492 15.67006042  1232
 
Satellite: STS-86      
Catalog number: 24964
Epoch time:      97276.96056061
Element set:      35
Inclination:       51.6525 deg
RA of node:       259.2033 deg
Eccentricity:    0.0017684
Arg of perigee:     1.2230 deg
Mean anomaly:     329.7492 deg
Mean motion:   15.67006042 rev/day
Decay rate:    7.80804e-05 rev/day^2
Epoch rev:             123
Checksum:              302
 
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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