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An artificial satellite is going round the earth, close to its surface. What is the time taken by it to complete one round? Given radius of the earth=6400 km.

An artificial satellite of the earth is to be established in the equatorial plane of the earth and to an observer at the equator it is required that the satellite will move eastward, completing one round trip per day. The distance of the satellite from the centre of the earth will be - ( The mass of the earth is 6.00 xx 10^(24) kg and its angular velocity = 7. 30 xx 10^(-5) "rad"//"sec". )

An artificial satellite revolves around the earth, remaining close to the surface of the earth, Show that its time period is T = 2pi sqrt(R_e/g)

A particle is moving in a circle of radius R in such a way that at any instant the normal and tangential component of the acceleration are equal. If its speed at t=0 is u_(0) the time taken to complete the first revolution is

A particle is moving in a circle of radius R in such a way that at any instant the normal and tangential components of the acceleration are equal. If its speed at t = 0 is u_(0) the time taken to complete the first revolution is :

A particle is moving in a circle of radius R in such a way that at any instant the normal and tangential components of the acceleration are equal. If its speed at t=0 is u_(0) the time taken to complete the first revolution is :