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N2WWD  > SAREX    29.11.96 07:08l 57 Lines 1866 Bytes #-10723 (0) @ AMSAT
BID : 1325_KC2FD
Read: GUEST OE7FMI
Subj: STS-80 Rev 138 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<DB0SON<DB0SIF<DB0AIS<DB0NDK<DB0ACH<ON4RAT<ON1ANR<
      PI8HWB<PI8VAD<PI8VNW<OH7RBA<OH2RBI<OH3RBR<PU3DTA<N2MEG<KB2VLX<N2BQF<
      KC2FD
Sent: 961128/0916Z @:KC2FD.#NLI.NY.USA.NA #:1325 [Coram, NY] $:1325_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:        96333.54506365700
                        11/28/1996  13:04:53.499 UTC
EFG E:                           16798875 ft
    F:                           14356762 ft
    G:                             154111 ft
    Edot:                       -13291.15 ft/s
    Fdot:                        15706.65 ft/s
    Gdot:                       -12036.63 ft/s
ndot/2 (drag):              0.00000497502 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        3.59301E-06 1/Earth Radii
Elset #:                               30
Rev @ Epoch:              138.49746414397
 
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   96333.54506366  .00000498  00000-0  35930-5 0   305
2 24660  28.4664 125.1873 0010105   6.1231 172.9633 15.72217460  1385
 
Satellite: STS-80      
Catalog number: 24660
Epoch time:      96333.54506366
Element set:      30
Inclination:       28.4664 deg
RA of node:       125.1873 deg
Eccentricity:    0.0010105
Arg of perigee:     6.1231 deg
Mean anomaly:     172.9633 deg
Mean motion:   15.72217460 rev/day
Decay rate:    4.97502e-06 rev/day^2
Epoch rev:             138
Checksum:              280
 
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
 
Ken Ernandes
n2wwd@amsat.org



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