7.Gravitation
normal

According to Kepler’s law the time period of a satellite varies with its radius as

A

${T^2} \propto {R^3}$

B

${T^3} \propto {R^2}$

C

${T^2} \propto (\frac{1}{R^3})$

D

${T^3} \propto (\frac{1}{R^2})$

Solution

According to Kepler's third law of planetary motion, "The square of a planet's orbital period is proportional to the cube of the length of the semimajor axis of its orbit."

So, $T ^2 \propto R ^3$

Standard 11
Physics

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