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OD5NZ > SAREX 24.03.96 20:06l 58 Lines 1768 Bytes #-11067 (0) @ WW
BID : 20_OD5NZ
Read: F5THQ DF5CH GUEST OE7FMI
Subj: STS-76 Rev 20 Orbital Data
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 20 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: 96083.54424537037
03/23/1996 13:03:42.800 UTC
EFG E: 10688547 ft
F: -12510558 ft
G: 14807904 ft
Edot: 21123.12 ft/s
Fdot: 5696.82 ft/s
Gdot: -10138.24 ft/s
ndot/2 (drag): 0.00002454196 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 5.28223E-06 1/Earth Radii
Elset #: 4
Rev @ Epoch: 20.33485701317
Launch was 22-MAR-96 / 08:13:04.073 UTC
Next Event is the NC-4 Burn at 23-MAR-96 / 23:52 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector using a 0.05 drag multiplier:
STS-76
1 23831U 96018A 96083.54424537 .00002454 00000-0 52822-5 0 47
2 23831 51.6484 193.1769 0117653 338.4650 142.1028 15.86399223 203
Satellite: STS-76
Catalog number: 23831
Epoch time: 96083.54424537
Element set: 4
Inclination: 51.6484 deg
RA of node: 193.1769 deg
Eccentricity: 0.0117653
Arg of perigee: 338.4650 deg
Mean anomaly: 142.1028 deg
Mean motion: 15.86399223 rev/day
Decay rate: 2.45420e-05 rev/day^2
Epoch rev: 20
Checksum: 304
VEC2TLE may be downloaded from:
ftp.amsat.org /amsat/software/PC/util
Ken Ernandes
n2wwd@amsat.org
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