OpenBCM V1.07b12 (Linux)

Packet Radio Mailbox

DB0FHN

[JN59NK Nuernberg]

 Login: GUEST





  
N2WWD  > SAREX    18.08.97 16:25l 73 Lines 1935 Bytes #-10360 (0) @ AMSAT
BID : 47168_KC2FD
Read: GUEST OE7FMI
Subj: STS-85 Rev 159 Orbital Data
Path: DB0RGB<DB0MAK<DB0SON<DB0SIF<DB0SRS<DB0ZDF<DB0HOM<DB0GE<LX0PAC<ON5VL<
      ON1ANR<PI8HWB<ON6AR<F6CNB<N9DBX<KB0TDF<N7VMR<WB0TAX<KE2VW<W2IM<KB2FAF<
      KA3VRW<N3DPU<WB3FYL<K3PGB<WA3TSW<K2ADJ<WT3V<KC2PB<WB2COP<WA2SNA<W2NRE<
      WA2PNU<N2BQF<KC2FD
Sent: 970817/1333Z @:KC2FD.#NLI.NY.USA.NOAM #:47168 [Coram_LI] $:47168_KC2FD



Message-Id: <47168_KC2FD@wb0tax.bbs>
Sender: n2wwd@kc2fd.#nli.ny.usa.noam
>From: n2wwd@kc2fd.#nli.ny.usa.noam


From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
To  : SAREX@AMSAT

Below is the current State Vector and Keplerian Elements for
STS-85.  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-85
Catalog Number:         24889  97039A
Epoch Date/Time:        97229.54323495400
                        08/17/1997  13:02:15.500 UTC
EFG E:                   16540492.0000000 ft
    F:                   6671089.00000000 ft
    G:                   12475781.0000000 ft
    Edot:                4271.32999999999 ft/s
    Fdot:                18548.4599999999 ft/s
    Gdot:                -15560.479999999 ft/s
ndot/2 (drag):              0.00320314481 rev/day^2
nddt/6:                       4.25652E-07 rev/day^3
Bstar:                        4.03480E-04 1/Earth Radii
Elset #:                               42
Rev @ Epoch:              159.38008093233

Launch: 07-AUG-97 / 14:41:00.082 UTC

The following Keplerian elements were computed by VEC2TLE from this
vector, using a 1.0 drag multiplier:

STS-85
1 24889U 97039A   97229.54323495  .00320314  42565-6  40348-3 0   425
2 24889  56.9934  30.5233 0008853 276.5372 220.3245 16.06837216  1594

Satellite: STS-85
Catalog number: 24889
Epoch time:      97229.54323495
Element set:      42
Inclination:       56.9934 deg
RA of node:        30.5233 deg
Eccentricity:    0.0008853
Arg of perigee:   276.5372 deg
Mean anomaly:     220.3245 deg
Mean motion:   16.06837216 rev/day
Decay rate:    3.20314e-03 rev/day^2
@poch rev:             159
Checksum:              315

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


 29.12.2025 20:58:54lGo back Go up