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A satellite of mass `m` orbits the earth in an elliptical orbit having aphelion distance `r_(a)` ad perihelion distance `r_(p)`. The period of the orbit is T. The semi-major and semi-minor axes of the ellipse are a and b respectively. The angular momentum of the satellite isA. `mpir_(a)//T`B. `2mpir_(a)//T`C. `mpiab//T`D. `2mpiab//T` |
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Answer» Correct Answer - D `L=2mdA//dt=2mpiab//T` |
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