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Mathematics, 29.01.2020 16:04 zay179

The formula to find the period of orbit of a satellite around a planet is (t^2) = (4pi^2/ gm) r3 where r is the orbit’s mean radius, m is the mass of the planet, and g is the universal gravitational constant. if you are given all the values except r, how do you rewrite the formula to solve for r?

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The formula to find the period of orbit of a satellite around a planet is (t^2) = (4pi^2/ gm) r3 whe...
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