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LW2EIQ > SAREX    02.07.96 03:03l 60 Lines 1884 Bytes #-10888 (0) @ AMSAT
BID : 16938_LW2EIQ
Read: GUEST OE7FMI
Subj: STS-78 Rev 132 Orbital Data
Path: DB0AAB<DB0MWS<DB0ZKA<DB0KCP<DB0CZ<HB9EAS<DB0GE<LX0PAC<ON5VL<ON4AIC<
      ON1AEO<ON6AR<F6CNB<PU3DTA<PP5AQ<CX2ACB<CX7BY<LW2EIQ
Sent: 960629/2259Z @:LW2EIQ.7600.BA.ARG.SA #:16938 [GF12FA] $:16938_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:        96180.79231481481
                        06/28/1996  19:00:56.000 UTC
EFG E:                          -17595666 ft
    F:                            1052907 ft
    G:                           12801568 ft
    Edot:                         2763.71 ft/s
    Fdot:                       -23346.00 ft/s
    Gdot:                         5731.13 ft/s
ndot/2 (drag):              0.00091087856 rev/day^2
nddt/6:                       3.45379E-08 rev/day^3
Bstar:                        1.45829E-04 1/Earth Radii
Elset #:                               28
Rev @ Epoch:              132.19166179309

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

The following Keplerian elements were computed by VEC2TLE from this
vector using a 1.5 drag multiplier:

STS-78
1 23931U 96036A   96180.79231481  .00091088  34538-7  14583-3 0   284
2 23931  39.0143 315.1849 0006775 329.8416  99.1569 16.02497897  1327

Satellite: STS-78
Catalog number: 23931
Epoch time:      96180.79231481
Element set:      28
Inclination:       39.0143 deg
RA of node:       315.1849 deg
Eccentricity:    0.0006775
Arg of perigee:   329.8416 deg
Mean anomaly:      99.1569 deg
Mean motion:   16.02497897 rev/day
Decay rate:    9.10879e-04 rev/day^2
Epoch rev:             132
Checksum:              351

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

Ken Ernandes
n2wwd@amsat.org



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