
Yefim S. answered 12/28/20
Math Tutor with Experience
GMm/r2 = mv2/r, where G is gravitational constant, M mass of Sun, m is mass of Mercury, r is distance from
Mercury to Sun, v is velocity of Mercury. From here v = (GM/r)1/2. = (6.67408·10-11·1.99·1030/(5.79·10^10))1/2 =
4.79·104m/s
Then orbital period of Mercury T = 2πr/v = 2π·5.79·1010m/(4.79·104m/s) = 7.595·106 s = 88 days