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Kepler's Third Law Calculator

Apply Kepler's third law, T² = 4π²a³/(GM), to solve for the orbital period, the semi-major axis, or the central mass. In solar-system units it reduces to T = √(a³/M), so a planet at 1 AU around a 1-solar-mass star orbits in one year.

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T = 2\pi\sqrt{\dfrac{a^3}{GM}} = \sqrt{\dfrac{a^3}{M}} = \sqrt{\dfrac{\left(1\,\text{au}\right)^3}{\left(1\,\text{M☉}\right)}} = ?\,\text{yr}

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