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Question

Using the fact that the mean radius of an elliptical orbit is the length of the semi-major axis, find the period of m2s orbit.
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Solution

Mean radius in this case will be

r=rmajor+rminor2=1×108+1.8×1082=1.4×108km

From Kepler's second law,

Tαr3/2

T1T2=r3/21r3/22=(11.4)3/2

T2=1.43/2(2)=3.31yr

Answer is 3.31yr

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