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

Question

3 years ago

15

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?

Mathematics

1 answer:

tatyana61 [14] · Answer 1 · 2022-05-22T14:46:04+03:00

tatyana61 [14]3 years ago

7 0

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