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Q. A satellite is launched into a circular orbit of radius $ r $ around the earth. A second satellite is launched into an orbit of radius $ 1.01 \,r $ . The period of the second satellite is larger than that of first one by approximately

UPSEEUPSEE 2010Gravitation

Solution:

Period of a satellite $T \propto r^{3 / 2}$
Hence, $\frac{\Delta T}{T}=\frac{3}{2} \frac{\Delta r}{r}$
As $\frac{\Delta r}{r}=\frac{1.01 r-r}{r}$
$=0.01=0.01 \times 100 \%=1 \%$
Hence, $\frac{\Delta T}{T}=\frac{3}{2} \times 1 \%=1.5 \%$