India's mangalyan was sent to the mars by launching it into a transfer orbit eom around the sun. it leaves the earth at e and meets mars at m. if the semi-major axis of earth's orbit is an e = 1.51011 m, that of mars's orbit am = 2.281011 m, taken kepler's laws give the estimate of time for mangalyan to reach mars from earth to be close to :
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2
I think it is about 1year
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6
320 days
Use this relationship to solve
T^2=r^3
where T is period of the orbit
r is radius of the orbit
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