OpenBCM V1.13 (Linux)

Packet Radio Mailbox

DB0FHN

[JN59NK Nuernberg]

 Login: GUEST





  
N2WWD  > SAREX    25.09.96 14:18l 59 Lines 1915 Bytes #-10790 (0) @ AMSAT
BID : 55646_KC2FD
Read: GUEST OE7FMI
Subj: STS-79 Rev 118 Orbital Data
Path: DB0AAB<DB0MWS<DB0RBS<DB0SEL<DB0ZDF<DB0AIS<DB0NDK<DB0ACH<ON4RAT<ON1ANR<
      PI8HWB<PI8VAD<PI8VNW<OH7RBA<OH3RBR<PU3DTA<WB0TAX<N4LXI<W3IXR<KD3AI<
      K3MJW<W3OC<WA3IOU<N8YIB<N2BQF<KC2FD
Sent: 960923/2111Z @:KC2FD.#NLI.NY.USA.NA #:55646 [Coram, NY] $:55646_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

 
         S T S - 7 9   O R B I T A L   D A T A
 
Below is the current State Vector and Keplerian Elements for STS-79.  
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-79
Catalog Number:         24324  96057A    
Epoch Date/Time:        96267.79342245370
                        09/23/1996  19:02:31.700 UTC
EFG E:                           10592310 ft
    F:                           19468409 ft
    G:                            1367008 ft
    Edot:                       -12909.59 ft/s
    Fdot:                         5620.13 ft/s
    Gdot:                        19685.97 ft/s
ndot/2 (drag):              0.00002988455 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        3.32715E-05 1/Earth Radii
Elset #:                               31
Rev @ Epoch:              118.01273989592
 
Launch was 16-SEP-96 / 08:54:49.062 UTC
 
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.5 drag multiplier:
 
STS-79      
1 24324U 96057A   96267.79342245  .00002988  00000-0  33272-4 0   313
2 24324  51.6511 347.1844 0012202 192.3566 172.2264 15.62077668  1188
 
Satellite: STS-79      
Catalog number: 24324
Epoch time:      96267.79342245
Element set:      31
Inclination:       51.6511 deg
RA of node:       347.1844 deg
Eccentricity:    0.0012202
Arg of perigee:   192.3566 deg
Mean anomaly:     172.2264 deg
Mean motion:   15.62077668 rev/day
Decay rate:    2.98845e-05 rev/day^2
Epoch rev:             118
Checksum:              317
 
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
 
Ken Ernandes
n2wwd@amsat.org


Read previous mail | Read next mail


 12.04.2026 01:30:55lGo back Go up