Two satellite revolve around the earth in circular orbits at heights `h_(1) and h_(2)` above the surface of the earth respectively. If R is radius of the earth, then the ratio of their orbital linear velocities is

Two satellites A and B of the same mass revolve around the earth in circular orbits. They are at heights of R and 3R respectively from the surface of the earth (R=radius of the earth). Find the ratio of their kinetic energies and potential energies.

An artificial satellite revolves around the earth in a circular orbit and is at a height of 300 km above the surface of the earth. Find the orbital speed and the time period of the satellite. The radius of the earth=6400 km, g=980 cm*s^(-2) .

Two identical satellites A and B revolve round the earth in circular orbits at distance R and 3R from the surface of the earth. The ratio of the linear momenta of A and B is (R = radius of the earth)

Two identical satellites A and B revolve round the earth in circular orbits at distance R and 3R from the surface of the earth. The ratio of the linear momenta of A and B is (R = radius of the earth)

An earth satellite of mass m revolves in a circular orbit at a height h from the surface of the earth. R is the radius of the earth and g is acceleration due to gravity at the surface of the earth. The velocity of the satellite in the orbit is given by

An earth satellite of mass m revolves in a circular orbit at a height h from the surface of the earth. R is the radius of the earth and g is acceleration due to gravity at the surface of the earth. The velocity of the satellite in the orbit is given by

A satellite of mass m_0 is revolving around the earth in circular orbit at a height of 3R from surface of the earth the areal velocity of satellite is (where R is radius of earth and M_0 is the mass of earth)

A satellite of mass m_0 is revolving around the earth in circular orbit at a height of 3R from surface of the earth the areal velocity of satellite is (where R is radius of earth and M_0 is the mass of earth)