OpenBCM V1.07b12 (Linux)

Packet Radio Mailbox

DB0FHN

[JN59NK Nuernberg]

 Login: GUEST





  
N2WWD  > SAREX    16.07.97 08:04l 60 Lines 1844 Bytes #-10394 (0) @ AMSAT
BID : 41959_KC2FD
Read: GUEST OE7FMI
Subj: STS-94 Rev 209 Orbital Data
Path: DB0RGB<DB0MAK<DB0SON<DB0ERF<DB0HSK<PI8DRS<ON4RAT<ON1ANR<PI8HWB<ON6AR<
      F6CNB<WU3V<WB0TAX<KC6UFM<KC5ELH<N2BQF<KC2FD
Sent: 970714/2238Z @:KC2FD.#NLI.NY.USA.NOAM #:41959 [Coram_LI] $:41959_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for
STS-94.  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-94
Catalog Number:         24849  97032A
Epoch Date/Time:        97195.79258680600
                        07/14/1997  19:01:19.500 UTC
EFG E:                   1029649.00000000 ft
    F:                   21435807.0000000 ft
    G:                   4335860.00000000 ft
    Edot:                -21271.659999999 ft/s
    Fdot:                -1228.4100000000 ft/s
    Gdot:                11002.4599999999 ft/s
ndot/2 (drag):              0.00058709627 rev/day^2
nddt/6:                       1.44540E-08 rev/day^3
Bstar:                        1.73148E-04 1/Earth Radii
Elset #:                               54
Rev @ Epoch:              209.06846177031

Launch: 01-JUL-97 / 18:02:00.063 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector and the scheduled launch time using a 2.0 drag multiplier:

STS-94
1 24849U 97032A   97195.79258681  .00058710  14454-7  17315-3 0   543
2 24849  28.4699 283.3700 0003839 116.4891 268.1711 15.91344789  2091

Satellite: STS-94
Catalog number: 24849
Epoch time:      97195.79258681
Element set:      54
Inclination:       28.4699 deg
RA of node:       283.3700 deg
Eccentricity:    0.0003839
Arg of perigee:   116.4891 deg
Mean anomaly:     268.1711 deg
Mean motion:   15.91344789 rev/day
Decay rate:    5.87096e-04 rev/day^2
Epoch rev:             209
Checksum:              371

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


 31.12.2025 02:52:36lGo back Go up