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OD5NZ > SAREX 08.03.96 12:55l 60 Lines 1838 Bytes #-11083 (0) @ AMSAT
BID : 34_OD5NZ
Read: OE5GMM DF5CH GUEST OE7FMI
Subj: STS-75 Rev 187 Orbital Data
Path: DB0AAB<DB0KCP<DB0ULM<DB0LX<DB0RBS<DB0HOM<DB0GE<LX0PAC<ON5VL<ON6RO<
OD5KU<OD5NZ
Sent: 960306/0927z @:OD5NZ.AMPR.ORG [Beirut, KM73SV] TCP/IP <> AX.25 Gateway #:
S T S - 7 5 O R B I T A L D A T A
Below is the rev 187 Earth-Fixed Greenwich (EFG) state vector for
STS-75. This vector data comes from NASA GSFC and was provided
courtesy of the DOD C-Band Radar Network.
Vector format = 117
Satellite Name: STS-75
Catalog Number: 23801 96012A
Epoch Date/Time: 96065.54402662037
03/05/1996 13:03:23.899 UTC
EFG E: -21378497 ft
F: -4144514 ft
G: -1820646 ft
Edot: 3014.96 ft/s
Fdot: -20621.66 ft/s
Gdot: 11921.17 ft/s
ndot/2 (drag): 0.00000787456 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 1.81492E-06 1/Earth Radii
Elset #: 29
Rev @ Epoch: 187.97243136726
Launch was 22-FEB-96 / 20:17:59.968 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.02 drag multiplier:
STS-75
1 23801U 96012A 96065.54402662 .00000787 00000-0 18149-5 0 291
2 23801 28.4465 199.2597 0008224 57.9292 292.1399 15.95915197 1870
Satellite: STS-75
Catalog number: 23801
Epoch time: 96065.54402662
Element set: 29
Inclination: 28.4465 deg
RA of node: 199.2597 deg
Eccentricity: 0.0008224
Arg of perigee: 57.9292 deg
Mean anomaly: 292.1399 deg
Mean motion: 15.95915197 rev/day
Decay rate: 7.87456e-06 rev/day^2
Epoch rev: 187
Checksum: 363
The next release of VEC2TLE will provide a feature to automatically
update your TLE or AMSAT Keplerian element file(s).
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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