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LW2EIQ > SAREX    07.07.96 08:11l 59 Lines 1883 Bytes #-10881 (0) @ AMSAT
BID : 17771_LW2EIQ
Read: DL2MEL GUEST OE7FMI
Subj: STS-78 Rev 223 Orbital Data
Path: DB0AAB<DB0KCP<DB0CZ<DB0GE<LX0PAC<ON7RC<ON1BWP<ON6AR<F6CNB<WB0TAX<
      PU3DTA<PY3PS<PY3SS<PY3KW<CX2ACB<CX7BY<LW2EIQ
Sent: 960705/2035Z @:LW2EIQ.7600.BA.ARG.SA #:17771 [GF12FA] $:17771_LW2EIQ
From: LW2EIQ@LW2EIQ.7600.BA.ARG.SA
To  : SAREX@AMSAT


         S T S - 7 8   O R B I T A L   D A T A

Below is the current State Vector and Keplerian Elements for STS-78.
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-78
Catalog Number:         23931  96036A
Epoch Date/Time:        96186.50026967593
                        07/04/1996  12:00:23.299 UTC
EFG E:                          -12169259 ft
    F:                           14573422 ft
    G:                          -10690725 ft
    Edot:                       -19943.77 ft/s
    Fdot:                        -9321.94 ft/s
    Gdot:                        10032.09 ft/s
ndot/2 (drag):              0.00225052131 rev/day^2
nddt/6:                       2.10598E-07 rev/day^3
Bstar:                        3.23710E-04 1/Earth Radii
Elset #:                               47
Rev @ Epoch:              223.85797306222

Launch was 20-JUN-96 / 14:49:00.093

The following Keplerian elements were computed by VEC2TLE from this
vector using a 3.3 drag multiplier:

STS-78
1 23931U 96036A   96186.50026968  .00225052  21060-6  32371-3 0   472
2 23931  39.0142 276.8025 0005281  12.9247 295.9452 16.04293661  2231

Satellite: STS-78
Catalog number: 23931
Epoch time:      96186.50026968
Element set:      47
Inclination:       39.0142 deg
RA of node:       276.8025 deg
Eccentricity:    0.0005281
Arg of perigee:    12.9247 deg
Mean anomaly:     295.9452 deg
Mean motion:   16.04293661 rev/day
Decay rate:    2.25052e-03 rev/day^2
Epoch rev:             223
Checksum:              304

VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util

Ken Ernandes
n2wwd@amsat.org


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