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Re: Satellite orbit procedure [message #29582]

Wed, 06 March 2002 06:50

Craig Markwardt
Messages: 1869
Registered: November 1996

Senior Member

Richard Lord <Richard.Lord@dlr.de> writes:
> 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.

Hi Richard--

This kind of code can also be found in the HELIO procedure in the IDL
Astronomy Library. You have to be aware that this kind of code is
only really good for bodies in the solar system. For near earth
objects the story is a little different. The so-called "mean" orbital
elements are also tied to an orbital model, like the SGP4. You would
need to propagate the orbit using this model.

Good luck,
Craig

--
------------------------------------------------------------ --------------
Craig B. Markwardt, Ph.D. EMAIL: craigmnet@cow.physics.wisc.edu
Astrophysics, IDL, Finance, Derivatives | Remove "net" for better response
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[Message index]

		Re: Satellite orbit procedure By: Craig Markwardt on Wed, 06 March 2002 06:50
		Re: Satellite orbit procedure By: Liam E. Gumley on Wed, 06 March 2002 06:58
		Re: Satellite orbit procedure By: Ed Wright on Thu, 28 February 2002 08:32

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