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OD5NZ > SAREX 25.03.96 01:52l 57 Lines 1750 Bytes #-11066 (0) @ WW
BID : 22_OD5NZ
Read: F5THQ DF5CH GUEST OE7FMI
Subj: STS-75 Corrected Rev 15 Orbital Message
Path: DB0AAB<DB0MFG<OE7XCI<IW3AQL<IN3TUR<IW3FPP<IW3GAE<IW3FHV<IW3GRX<IW1BBL<
IK1MSL<I1NHK<I1DEP<IW2KTL<IW2KTL<IK2FMJ<I4EUM<IK5CKL<IK5MEP<I5SGG<
OD5RAK<OD5ET<OD5KU<OD5NZ
Sent: 960323/2120z @:OD5NZ.LBN.MDLE [Beirut, KM73SV] TCP/IP <> AX.25 Gateway #:
S T S - 7 6 O R B I T A L D A T A
Below is the rev 15 Earth-Fixed Greenwich (EFG) state vector for
STS-76. This vector data comes from NASA GSFC and was provided
courtesy of the DOD C-Band Radar Network.
Vector format = 117
Satellite Name: STS-76
Catalog Number: 23831 96018A
Epoch Date/Time: 96083.20845486100
03/23/1996 05:00:10.499 UTC
EFG E: 8247470.00000000 ft
F: -19838255.000000 ft
G: -3014856.0000000 ft
Edot: 14380.6399999999 ft/s
Fdot: 2995.19999999999 ft/s
Gdot: 19719.0099999999 ft/s
ndot/2 (drag): 0.00008217600 rev/day^2
nddt/6: 2.80704E-10 rev/day^3
Bstar: 1.06745E-05 1/Earth Radii
Elset #: 3
Rev @ Epoch: 14.97180804547
Launch was 22-MAR-96 / 08:13:04.073 UTC
Next Event is the NC-4 Burn at 23-MAR-96 / 15:39 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.1 drag multiplier:
STS-76
1 23831U 96018A 96083.20845486 .00008218 28070-9 10675-4 0 38
2 23831 51.6487 194.9628 0046286 346.3208 3.5377 16.03983913 144
Satellite: STS-76
Catalog number: 23831
Epoch time: 96083.20845486
Element set: 3
Inclination: 51.6487 deg
RA of node: 194.9628 deg
Eccentricity: 0.0046286
Arg of perigee: 346.3208 deg
Mean anomaly: 3.5377 deg
Mean motion: 16.03983913 rev/day
Decay rate: 8.21760e-05 rev/day^2
Epoch rev: 14
Checksum: 324
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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