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N2WWD  > SAREX    03.10.97 04:56l 76 Lines 2017 Bytes #-10313 (0) @ AMSAT
BID : 3896_EA3CXF
Read: GUEST OE7FMI
Subj: STS-86 Rev 58 Orbital Data
Path: DB0AAB<DB0CRL<DB0TTM<DB0SWR<DB0RBS<DB0PSC<DB0ACH<ON4RAT<ON1ANR<ON6AR<
      F6CNB<WB0TAX<EA3CIW<EA3CWZ<EA3CXF
Sent: 971003/0102z @:EA3CXF.EAB.ESP.EU [ARU] {EANET3.05}] #:101995 $:3896_EA3CX

Message-Id: 3896_ea3cxf
From: wb0tax@ea3cxf.eab.esp.eu 
To: sarex@amsat



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 Docked
Catalogumber:         24964  97055A    
Epoch Date/Time:        97272.79439467600
                   /1997  19:03:55.700 UTC
EFG E:                   12253461.0000000 ft
    F:                   -13510643.000000 ft
    G:                   -12682251.000000 ft
    Edot:                19418.0999999999 ft/s
    Fdot:                4911.34000000000 ft/s
    Gdot:                13530.0799999999 ft/s
ndot/2 (drag):              0.00005589333 rev/day^2
nddt/6:                       1.33496E-10 rev/day^3
Bstar:                        6.68632E-05 1/Earth Radii
Elset #:                               18
Rev @ Epoch:               58.87024911869
 
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 Docked
1 24964U 97055A   97272.79439468  .00005589  13350-9  66863-4 0   181
2 24964  51.6536 280.1625 0004519 172.2218 141.0902 15.60302746   583
 
Satellite: STS-86 Docked
Catalog number: 24964
Epoch time:      97272.79439468
Element set:      18
Inclination:       51.6536 deg
RA of node:       280.1625 deg
Eccentricity:    0.0004519
Arg of perigee:   172.2218 deg
Mean anomaly:     141.0902 deg
Mean motion:   15.60302746 rev/day
Decay rate:    5.58933e-05 rev/day^2
Epoch rev:              58
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
 
 
 







{Mensaje distribuido por: EANET (EA3HCC-5: Conectate al Cluster de Barcelona)}


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