A satellite is launched into a circular orbit | vedclass

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Question

${T}^{2} \propto R^{3}$

$T=k R^{3 / 2}$

$\frac{d T}{T}=\frac{3}{2} \frac{d R}{R}$

$=\frac{3}{2} 	imes 0.02=0.03$

$\% 	ext { Change }=3 \

Vedclass · Accepted Answer

$3.0$

Vedclass · Answer

${T}^{2} \propto R^{3}$

$T=k R^{3 / 2}$

$\frac{d T}{T}=\frac{3}{2} \frac{d R}{R}$

$=\frac{3}{2} 	imes 0.02=0.03$

$\% 	ext { Change }=3 \,\%$

A satellite is launched into a circular orbit of radius $R$ around earth, while a second satellite is launched into a circular orbit of radius $1.02\, {R}$. The percentage difference in the time periods of the two satellites is -

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