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Satellite orbit procedure [message #29668] Thu, 28 February 2002 05:32
Richard Lord is currently offline  Richard Lord
Messages: 1
Registered: February 2002
Junior Member
Hi,

I'm looking for a procedure that takes as input the parameters of a
satellite orbit (Kepler orbit parameters), and outputs so-called
statevectors. A statevector contains the x,y,z and vx,vy,vz
coordinates at any particular point in time.

If anybody has seen a procedure that does something along the lines
explained above, I would be grateful to receive a copy.

Thanks in advance,
Richard

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