if the radius of the earths orbit around the sun is R and the time period of the revolution of the earth around the sun is T the mass of sun is
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Kepler’s third law is written as P^2 = 4 pi^2 a^3 / (GM)
Where P = T is the orbital period, a = R is the mean distance of the planet from the sun, M is the mass of the sun, and G is the gravitational constant. Therefore,
M = 4 pi^2 R^3 / (GT^2).
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