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Satellite orbit around Earth Simultation with Matlab!

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Uploaded on Nov 11, 2009

Check my new video with actual rotating earth at :

http://www.youtube.com/watch?v=Lobo56...

Inital parameters:
R=[6472.7,-7470.8,-2409.3] km
V=[3.9914,2.7916,-3.2948] km/s
Values Calculated:
inc=34.9398 deg
raan=110.4872 deg
e=0.2444
true anamoly=130.42 deg
radius at perigee=6.8799 e 3 km
semi major axis=9.1056 e 3 km
Period=8647.1 sec

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