A satellite is in a circular orbit around Earth at an altitude of 650 km. What orbital speed must the satellite maintain to stay in orbit at this altitude?

Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 409 km above the earth’s surface, while that for satellite B is at a height of 835 km. Find the orbital speed for (a) satellite A and (b) satellite B.

a) What is the total energy needed to place a 2.0 x 103 kg satellite into circular Earth orbit at an altitude of 5.0 x 102 km? b) How much additional energy would have to be supplied to the satellite once it was in orbit, to allow it to escape from Earth’s gravitational field?

A particular satellite was placed in a circular orbit about 216 mi above Earth. (a) Determine the orbital speed of the satellite. m/s (b) Determine the time required for one complete revolution. min Submit Answer

A centripetal force of 200 N acts on a 1,000-kg satellite moving with a speed of 5,000 m/s in a circular orbit around a planet. What is the radius of its orbit?

A satellite of mass 390 kg is in a circular orbit around the Earth at an altitude equal to the Earth's mean radius. Find the satellite's orbital speed.

A satellite is orbiting earth  at a distance of  3.1 X 105 m above the surface of the Earth. What is its orbital speed? (G = 6.67 X 10-11 Nm2/Kg2; M of Earth = 5.97 x 10 24 kg; Radius of Earth = 6.37 x 10 6 m)

Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 497 km above the earth's surface, while that for satellite B is at a height of 752 km. Find the orbital speed for (a) satellite A and (b) satellite B.

Calculate the speed of a 525.0 kg satellite in orbit 200.0 km above the surface of Earth.

A satellite traveling in a circular orbit 1569 km above the surface of a planet takes 2.3 hours to make an orbit. The radius of the planet is approximately 5518 km. Find the linear speed of the satellite in kilometers per hour.