A satellite of mass m is orbiting around the earth (mass M, radius R) in a circular orbital of radius 4R. It starts losing energy slowly at a constant `-(dE)/(dt)=eta`due to friction. Find the time (t) in which the satellite will spiral down to the surface of the earth.

A satellite of mass M_(s) is revolving around the earth (Mass M) in a orbit of radius R. Find its angular momentum.

A satellite of mass M_(S) is orbitting the earth in a circular orbit of radius R_(S) . It starts losing energy slowly at a constant rate C due to friction if M_(e) and R_(e) denote the mass and radius of the earth respectively show that the satellite falls on the earth in a limit time t given by t=(GM_(S)M_(e))/(2C)((1)/(R_(e))-(1)/(R_(S)))

A satellite of mass M_(S) is orbitting the earth in a circular orbit of radius R_(S) . It starts losing energy slowly at a constant rate C due to friction if M_(e) and R_(e) denote the mass and radius of the earth respectively show that the satellite falls on the earth in a limit time t given by t=(GM_(S)M_(e))/(2C)((1)/(R_(e))-(1)/(R_(S)))

A satellite of mass M_(S) is orbitting the earth in a circular orbit of radius R_(S) . It starts losing energy slowly at a constant rate C due to friction if M_(e) and R_(e) denote the mass and radius of the earth respectively show that the satellite falls on the earth in a limit time t given by t=(GM_(S)M_(e))/(2C)((1)/(R_(e))-(1)/(R_(S)))

A satellite of mass m is orbiting the earth in a circular orbit of radius r . It starts losing energy due to small air resistance at the rate of C J//s . Then the time teken for the satellite to reach the earth is...........

A satellite of mass m is orbiting the earth in a circular orbit of radius r . It starts losing energy due to small air resistance at the rate of C J//s . Then the time teken for the satellite to reach the earth is...........

A satellite of mass m is orbiting the earth in a circular orbit of radius r . It starts losing energy due to small air resistance at the rate of C J//s . Then the time teken for the satellite to reach the earth is...........

A satellite of mass m is orbiting around the earth at a height equal to twice the radius of the earth (R). Its potential energy is given by