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Mathematics, 22.11.2019 16:31 yoongislaugh

The formula to find the period of orbit of a satellite around a planet is t2=(4π2gm)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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