OpenBCM V1.13 (Linux)

Packet Radio Mailbox

DB0FHN

[JN59NK Nuernberg]

 Login: GUEST





  
N2WWD  > SAREX    23.02.97 00:37l 61 Lines 1854 Bytes #-10628 (0) @ AMSAT
BID : 13464_KC2FD
Read: GUEST OE7FMI
Subj: STS-82 Rev 143 Orbital Data
Path: DB0AAB<DB0PV<DB0MAK<OK0PKL<OK0PPR<OK0PRG<OK0PAB<OH3RBR<OH2RBI<OH2RBJ<
      OH1RBD<OH1RBU<OH1RBF<OH6RBT<OH6RDP<OH6RBC<OH6RDC<OH6RBV<OH6RBG<SK2AT<
      SK2DR<WB0TAX<N4LXI<W3IXR<KD3AI<W3OC<WA3IOU<N8YIB<N2BQF<KC2FD
Sent: 970221/0335Z @:KC2FD.#NLI.NY.USA.NA #:13464 [Coram_LI] $:13464_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for STS-82.  
The vector data comes from NASA; the Keplerian Elements were 
computed from the vector.  
 
This file may be read by VEC2TLE version 9648 to update your 
Keplerian Elements text file.
 
Vector format = 117
Satellite Name:         STS-82
Catalog Number:         24719  97004A    
Epoch Date/Time:        97051.91688425900
                        02/20/1997  22:00:18.799 UTC
EFG E:                   1232759.00000000 ft
    F:                   -22260594.000000 ft
    G:                   -5224219.0000000 ft
    Edot:                20864.5400000000 ft/s
    Fdot:                -1214.4000000000 ft/s
    Gdot:                10400.8400000000 ft/s
ndot/2 (drag):              0.00000210425 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        2.16680E-05 1/Earth Radii
Elset #:                               41
Rev @ Epoch:              143.92148564665
 
Launch occurred: 11-FEB-97 / 08:55:17.087 UTC
 
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.5 drag multiplier:
 
STS-82      
1 24719U 97004A   97051.91688426  .00000210  00000-0  21668-4 0   417
2 24719  28.4704  59.7376 0024284  64.2630 267.4579 14.89102017  1439
 
Satellite: STS-82      
Catalog number: 24719
Epoch time:      97051.91688426
Element set:      41
Inclination:       28.4704 deg
RA of node:        59.7376 deg
Eccentricity:    0.0024284
Arg of perigee:    64.2630 deg
Mean anomaly:     267.4579 deg
Mean motion:   14.89102017 rev/day
Decay rate:    2.10425e-06 rev/day^2
Epoch rev:             143
Checksum:              312
 
VEC2TLE may be downloaded from:
 
http://www.amsat.org/amsat/sarex/orbit.html
 
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
 
 


Read previous mail | Read next mail


 31.03.2026 12:19:14lGo back Go up