OpenBCM V1.13 (Linux)

Packet Radio Mailbox

DB0FHN

[JN59NK Nuernberg]

 Login: GUEST





  
N2WWD  > SAREX    18.05.97 17:53l 65 Lines 2078 Bytes #-10540 (0) @ AMSAT
BID : 32047_KC2FD
Read: GUEST OE7FMI
Subj: STS-84 Rev 12 Orbital Data
Path: DB0AAB<DB0KCP<DB0GPP<DB0LX<DB0RBS<DB0SWR<DB0FP<DB0SRS<DB0MW<DB0AIS<
      DB0NDK<DB0ACH<ON4RAT<ON1ANR<ON6AR<F6CNB<WB0TAX<PU3DTA<N2MEG<KB2VLX<
      WA2SNA<WA2AWG<N2BQF<KC2FD
Sent: 970516/0236Z @:KC2FD.#NLI.NY.USA.NA #:32047 [Coram_LI] $:32047_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NA
To  : SAREX@AMSAT

STS-84
1 24804U 97023A   97135.99132986  .00018215  13865-8  43944-4 0    33
2 24804  51.6566 247.7997 0014290 339.6311 201.1570 15.95444273   129
 
Launch time for STS-84: 15 MAY 97 @ 08:07:48.076 UTC
 
Earth-Fixed Greenwich State Vector:
 
Vector format = 117
Satellite Name:         STS-84
Catalog Number:         24804  97023A
Epoch Date/Time:        97135.99132986100
                        05/15/1997  23:47:30.899 UTC
EFG E:                   -20861539.000000 ft
    F:                   -6657211.0000000 ft
    G:                   -248727.00000000 ft
    Edot:                4499.72999999999 ft/s
    Fdot:                -13387.370000000 ft/s
    Gdot:                -19883.610000000 ft/s
ndot/2 (drag):              0.00018214606 rev/day^2
nddt/6:                       1.38649E-09 rev/day^3
Bstar:                        4.39437E-05 1/Earth Radii
Elset #:                                3
Rev @ Epoch:               12.50219131239
 
Keplerian Elements (Amsat format):
 
Satellite: STS-84
Catalog number: 24804
Epoch time:      97135.99132986
Element set:       3
Inclination:       51.6566 deg
RA of node:       247.7997 deg
Eccentricity:    0.0014290
Arg of perigee:   339.6311 deg
Mean anomaly:     201.1570 deg
Mean motion:   15.95444273 rev/day
Decay rate:    1.82146e-04 rev/day^2
Epoch rev:              12
Checksum:              314
 
SPACE SHUTTLE ORBITAL DATA:
 
These 2-line elements have been generated using Ken Ernandes' program
VEC2TLE using real time state vector data supplied by DOD C-Band Radar
Network courtesy Dave Simonson. Note that the epoch of the 2-line
elements is the same as the state vector time.
 
Drag and B-Star parameters are internally calculated by VEC2TLE using
a drag factor of 0.5. Rev numbers use NASA orbit numbering convention.
 
                                   Dave Ransom
                                   RPV Astronomy BBS
                                   http://www.dransom.com
 
----------
David H. Ransom, Jr.   Email:rans7500@spacelink.msfc.nasa.gov
 
 



Read previous mail | Read next mail


 28.03.2026 15:31:48lGo back Go up