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AMSAT OSCAR 40 Estimated Keplerian Element Set #5
- Subject: [amsat-bb] AMSAT OSCAR 40 Estimated Keplerian Element Set #5
- From: "Kenneth J. Ernandes" <n2wwd@xxxxxxxxxxxxxx>
- Date: Fri, 8 Dec 2000 08:37:28 -0500
Below is the current state vector and Keplerian element estimate for
AMSAT OSCAR 40.
Vector format = 7
Satellite Name: AO-40 / OSCAR 40
Catalog Number: 26609 00072B
Epoch Date/Time: 343.50000000000
12/08/2000 12:00:00.000 UTC
ECI X: -11200.159135575 km
Y: -43794.661976426 km
Z: 1345.53214763604 km
Xdot: 1.57306794064000 km/s
Ydot: -0.0192097725400 km/s
Zdot: 0.15371053026000 km/s
ndot/2 (drag): 0.00000000690 rev/day^2
nddt/6: 0.00000E+00 rev/day^3
Bstar: 1.23081E-05 1/Earth Radii
Elset #: 5
Rev @ Epoch: 45.09033523945
The following Keplerian elements were computed from this vector:
AO-40 / OSCAR 40
1 26609U 00072B 00343.50000000 .00000001 00000-0 12308-4 0 54
2 26609 6.3783 240.2081 7347480 190.5533 201.9831 2.03015472 455
Satellite: AO-40 / OSCAR 40
Catalog number: 26609
Epoch time: 00343.50000000
Element set: 5
Inclination: 6.3783 deg
RA of node: 240.2081 deg
Eccentricity: 0.7347480
Arg of perigee: 190.5533 deg
Mean anomaly: 201.9831 deg
Mean motion: 2.03015472 rev/day
Decay rate: 6.90000e-09 rev/day^2
Epoch rev: 45
Checksum: 239
Ken Ernandes, N2WWD
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
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