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How does one derive the total energy in an elliptic orbit:
E= - \frac{GMm}{2a}
where a is the semi-major axis?
I did manage to get the result for the special case of circular orbit, as
v = \sqrt{\frac{GM}{R}}
But the problem is that I can't figure out a way to express v in an elliptic orbit.
If at all possible, give hints (that is: not a direct answer), as I'd rather try it myself first :).
E= - \frac{GMm}{2a}
where a is the semi-major axis?
I did manage to get the result for the special case of circular orbit, as
v = \sqrt{\frac{GM}{R}}
But the problem is that I can't figure out a way to express v in an elliptic orbit.
If at all possible, give hints (that is: not a direct answer), as I'd rather try it myself first :).
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