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N2WWD  > SAREX    21.11.96 11:20l 62 Lines 1920 Bytes #-10732 (0) @ AMSAT
BID : 31_KC2FD
Read: DK8TG GUEST OE7FMI
Subj: STS-80 Rev 1 Orbital Data
Path: DB0AAB<DB0FSG<DB0IGL<DB0KCP<DB0ULM<DB0LX<DB0RBS<DB0SEL<DB0ZDF<DB0GE<
      LX0PAC<ON7RC<ON4AWP<ON6AR<F6CNB<K5ARH<WU3V<WB0TAX<N4LXI<W3IXR<KD3AI<
      W3OC<WA3IOU<N8YIB<N2BQF<KC2FD
Sent: 961119/1928Z @:KC2FD.#NLI.NY.USA.NA #:31 [Coram, NY] $:31_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

 
         S T S - 8 0   O R B I T A L   D A T A
 
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 = 1017
Satellite Name:         STS-80
Catalog Number:         24660  96065A    
Epoch Date/Time:        96324.91602078700
                        11/19/1996  21:59:04.195 UTC
ECI X:                     20050390.21857 ft
M50 Y:                     8608824.672273 ft
    Z:                    -3322029.606573 ft
    Xdot:                    -10472.16406 ft/s
    Ydot:                     19964.80469 ft/s
    Zdot:                    -11419.40234 ft/s
ndot/2 (drag):              0.00005016165 rev/day^2
nddt/6:                       1.06802E-10 rev/day^3
Bstar:                        3.63978E-05 1/Earth Radii
Elset #:                                1
Rev @ Epoch:                2.54975393664
 
Launch was 19-NOV-96 / 19:55:47.060 UTC
 
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.5 drag multiplier:
 
STS-80      
1 24660U 96065A   96324.91602079  .00005016  10680-9  36398-4 0    15
2 24660  28.4671 187.9703 0008324 259.1359 298.7861 15.72131467    24
 
Satellite: STS-80      
Catalog number: 24660
Epoch time:      96324.91602079
Element set:       1
Inclination:       28.4671 deg
RA of node:       187.9703 deg
Eccentricity:    0.0008324
Arg of perigee:   259.1359 deg
Mean anomaly:     298.7861 deg
Mean motion:   15.72131467 rev/day
Decay rate:    5.01617e-05 rev/day^2
Epoch rev:               2
Checksum:              308
 
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
 
Ken Ernandes
n2wwd@amsat.org
 




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