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

The height h of the satellite above the earth s surface is take radius of earth as r e.

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

The orbital velocity of an artificial satellite in a circular orbit just above the centre s surface is v. The period of the earth as it travels around the sun is one year. In space gravity supplies the centripetal force that causes satellites like the moon to orbit larger bodies like the earth. If you know the satellite s speed and the radius at which it orbits you can figure out its period.

You can calculate the speed of a satellite around an object using the equation. 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 initial velocity imparted is horizontal. The orbital velocity of a satellite orbiting at an altitude of half of the radius is.

By steven holzner. 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 orbital velocity of an artificial satellite in a circular orbit just above the earth s surface is v 0. What would be the maximum distance of the satellite from the earth when it is in the orbit.