(adsbygoogle = window.adsbygoogle || []).push({}); 1. The problem statement, all variables and given/known data

The period of a comet orbit is 100 years. As its closests approach is 0.37 AU from the sun. What is the semi-major axis of the comet's orbit? How far does it get from the sun?

2. Relevant equations

(T1/T2)^2 = (s1/s2)^3

3. The attempt at a solution

I dont even know where to begin with this problem any help would be really appreciated.

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# Elliptical Orbit

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