Elliptical orbit parameterized by time

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DuckAmuck
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TL;DR
How to express an eliptical orbit in terms of time
It is fairly trivial to do this with a circular orbit: $$(x,y) = (cos(\omega t),sin(\omega t))$$
where t is time, and $$\omega = \sqrt{GM/r^3}$$
How this parametric equation look for an elliptical orbit?
 
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DuckAmuck said:
Summary:: How to express an eliptical orbit in terms of time

It is fairly trivial to do this with a circular orbit: $$(x,y) = (cos(\omega t),sin(\omega t))$$
where t is time, and $$\omega = \sqrt{GM/r^3}$$
How this parametric equation look for an elliptical orbit?

I don't think it works out very well. Have you tried?
 
Yes. I get something non-analytic.
 
DuckAmuck said:
Yes. I get something non-analytic.
I think that's what you get. The analysis from Newton's laws bails out at a certain point and describes the shape of an orbit in terms of ##r## and ##\theta##, but eliminates ##t##. You get the shape (ellipse) and the period, but not an analytic formula for position as a function of time.
 
Look up "The Kepler Equation". You're in for an interesting ride!
 
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gneill said:
Look up "The Kepler Equation". You're in for an interesting ride!
Thank you!