Kepler's Law
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A satellite which is geostationary in a particular orbit is taken to another orbit. Its distance from the centre of earth in new orbit is 2 times that of the earlier orbit. The time period in the second orbit is
4.8 hours
48√2 hours
24 hours
24√2 hours
Kepler's second law regarding constancy of aerial velocity of a planet is a consequence of the law of conservation of
Energy
Linear momentum
None of these
Angular momentum
When a satellite in a circular orbit around the earth enters the atmospheric region, it encounters small air resistance to its motion. Then -
Its kinetic energy remains constant
Its kinetic energy decreases
Its angular momentum about the earth decreases
Its period of revolution around the earth increases
A satellite of mass m moves along an elliptical path around the earth. The areal velocity of the satellite is proportional to
m-1
m0
m1/2
m
If a body describes a circular motion under inverse square field, the time taken to complete one revolution, T is related to the radius of the circular orbit as