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How do you calculate centripetal acceleration of a satellite in orbit around a planet?
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- bonoboLv 71 decade agoFavorite Answer
Fc = M • V² ⁄ R = M • a
a = V² ⁄ R
where R = (Re + h)
Re = radius of the earth (m)
h = altitude of satellite (m)
V = velocity (m/sec)
M = mass (Kg)
- Anonymous1 decade ago
I don't actually .. just let them follow their course
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