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A satellite is revolving round the earth in a circular orbit of radius r and velocity v0. A particle is projected from the satellite in forward direction with relative velocity v = ((5/4) - 1)v0. Calculate its minimum and maximum distances from earth's centre during subsequent motion of the particle.

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Since, vp lies between orbital velocity and escape velocity, path of the particle would be an ellipse with r being the minimum distance.

Let r' be the maximum distance and v'p its velocity at that moment.

Then from conservation of angular momentum and conservation of mechanical energy, we get 

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