derivation of time period of satelite
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I've worked it out again, this is my working:
I put Newton's law of gravitation and the centripetal force equation equal to each other:
GMmr2=mv2r
Multiply both sides by r:
GMmr=mv2
Sub in v=2πrT for v:
GMmr=m(2πrT)2
Divide both sides by m:
GMr=(2πrT)2
Root both sides:
GMr−−−√=2πrT
Flip both sides and divide by 2πr:
T=2πrGMr√
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