The Orbital Velocity Of An Artificial Satellite In A Circular Orbit Just Above

A satellite is put in an orbit just above the earth s atmosphere with a velocity sqrt 1 5 times the velocity for a circular orbit at the that height.

The orbital velocity of an artificial satellite in a circular orbit just above.

By steven holzner. The initial velocity imparted is horizontal. An artificial satellite is moving in a circular orbit around the earth with a speed equal to half the magnitude of the escape velocity from the earth. In space gravity supplies the centripetal force that causes satellites like the moon to orbit larger bodies like the earth.

The orbital velocity of an artificial satellite in a circular orbit just above the centre s surface is v. The orbital velocity of an artificial satellite in a circular orbit just above the earth s surface is v 0. If you know the satellite s speed and the radius at which it orbits you can figure out its period. Thanks to physics if you know the mass and altitude of a satellite in orbit around the earth you can calculate how quickly it needs to travel to maintain that orbit.

The period of the earth as it travels around the sun is one year. The height h of the satellite above the earth s surface is take radius of earth as r e. For a satellite orbiting at an altitude of half 1705911. The orbital velocity of a satellite orbiting at an altitude of half of the radius is.