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N2WWD  > SAREX    26.11.96 16:34l 57 Lines 1866 Bytes #-10726 (0) @ AMSAT
BID : 947_KC2FD
Read: GUEST OE7FMI
Subj: STS-80 Rev 96 Orbital Data
Path: DB0AAB<DB0KCP<DB0ULM<DB0LX<DB0RBS<DB0SEL<DB0ZDF<DB0AIS<DB0NDK<DB0ACH<
      ON4RAT<ON1ANR<ON6AR<F6CNB<PU3DTA<N2MEG<KB2VLX<WA2AAR<WA2JVM<WA2SNA<
      WA2AWG<N2BQF<KC2FD
Sent: 961125/2059Z @:KC2FD.#NLI.NY.USA.NA #:947 [Coram, NY] $:947_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) 262-6782 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:        96330.86544444400
                        11/25/1996  20:46:14.399 UTC
EFG E:                          -12377638 ft
    F:                          -15085367 ft
    G:                           10319245 ft
    Edot:                        17536.99 ft/s
    Fdot:                       -16001.15 ft/s
    Gdot:                        -2307.72 ft/s
ndot/2 (drag):              0.00000485469 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        3.65357E-06 1/Earth Radii
Elset #:                               22
Rev @ Epoch:               96.28055925232
 
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   96330.86544444  .00000485  00000-0  36536-5 0   226
2 24660  28.4670 144.6882 0007677   2.5344  98.4600 15.71280193   964
 
Satellite: STS-80      
Catalog number: 24660
Epoch time:      96330.86544444
Element set:      22
Inclination:       28.4670 deg
RA of node:       144.6882 deg
Eccentricity:    0.0007677
Arg of perigee:     2.5344 deg
Mean anomaly:      98.4600 deg
Mean motion:   15.71280193 rev/day
Decay rate:    4.85469e-06 rev/day^2
Epoch rev:              96
Checksum:              320
 
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
 
Ken Ernandes
n2wwd@amsat.org



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