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N2WWD  > SAREX    09.12.96 21:36l 63 Lines 1872 Bytes #-10710 (0) @ AMSAT
BID : 3156_KC2FD
Read: GUEST OE7FMI
Subj: STS-80 Rev 278 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<DB0SON<DB0SIF<DB0SRS<DB0ZDF<DB0GE<LX0PAC<ON7RC<
      ON1BWP<ON6AR<ON1ANR<PI8HWB<PI8VAD<PI8VNW<OH7RBA<OH2RBI<OH2RBJ<OH1RBD<
      OH1RBU<OH0RBA<SM0GJK<SM0ETV<KA0WIN<KI4ZJ<K4VJI<KD4IDR<WB0TAX<PU3DTA<
      N2MEG<KB2VLX<N2BQF<KC2FD
Sent: 961207/0832Z @:KC2FD.#NLI.NY.USA.NA #:3156 [Coram, NY] $:3156_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for STS-80.  
The vector data comes from NASA; the orbital parameters were computed 
from the vector.  Hourly vector updates are available from NASA GSFC 
OIG RAID RBBS at (301) 262-6784 or by telnet: oig1.gsfc.nasa.gov 
(UserID = oig / Password = goddard1).
 
Vector format = 117
Satellite Name:         STS-80
Catalog Number:         24660  96065A    
Epoch Date/Time:        96342.41765393500
                        12/07/1996  10:01:25.299 UTC
EFG E:                   4249534.00000000 ft
    F:                   -18828707.000000 ft
    G:                   10457379.0000000 ft
    Edot:                23360.6699999999 ft/s
    Fdot:                5418.53999999999 ft/s
    Gdot:                200.539999999999 ft/s
ndot/2 (drag):              0.00000642833 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        4.02239E-06 1/Earth Radii
Elset #:                               60
Rev @ Epoch:              278.24754879730
 
Launch was 19-NOV-96 / 19:55:47.060 UTC
 
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.05 drag multiplier:
 
STS-80      
1 24660U 96065A   96342.41765393  .00000643  00000-0  40224-5 0   605
2 24660  28.4698  60.6834 0042587 104.9065 344.2119 15.74248646  2783
 
Satellite: STS-80      
Catalog number: 24660
Epoch time:      96342.41765393
Element set:      60
Inclination:       28.4698 deg
RA of node:        60.6834 deg
Eccentricity:    0.0042587
Arg of perigee:   104.9065 deg
Mean anomaly:     344.2119 deg
Mean motion:   15.74248646 rev/day
Decay rate:    6.42833e-06 rev/day^2
Epoch rev:             278
Checksum:              333
 
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
 
Ken Ernandes
n2wwd@amsat.org







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