Time Period Of A Satellite

Near the earth surface time period of the satellite.

Time period of a satellite.

Time taken by the satellite to complete one revolution round the earth is called time period. The orbital period is the time a given astronomical object takes to complete one orbit around another object and applies in astronomy usually to planets or asteroids orbiting the sun moons orbiting planets exoplanets orbiting other stars or binary stars. A satellite close to the earth is in orbit above the equator with a period of revolution of 1. 5 h o u r s in the same sense as that of the earth.

If it is above a point p on the equator at some time it will be above p again after a time. The period of the earth as it travels around the sun is one year. Calculates the orbital radius and period and flight velocity from the orbital. And r r h radius of the earth height of the satellite from the surface of the earth.

If you know the satellite s speed and the radius at which it orbits you can figure out its period. The time taken by the satellite to complete one revolution around the planet is known as the period of revolution of the satellite. Expression for period of a satellite. T 2π r g 5 08 10 3 s 84 min.

Period of a satellite. T 2π r 3 gm 2π r h 3 g g gm r 2. The period of a satellite t and the mean distance from the central body r are related by the following equation. Time period t circumference of the orbit orbital velocity.

For objects in the solar system this is often referred to as the sidereal period determined by a 360 revolution of one celestial. Where t is the period of the satellite r is the average radius of orbit for the satellite distance from center of central planet and g is 6 673 x 10 11 n m 2 kg 2. Time period of revolution of earth satellite. T 2πr v 0 2π r h v 0.

Say period of revolution is t and the radius of the orbit is r. It is denoted by t. T 2π r 3 gm 3π gp. Time period of a satellite.

Geostationary or parking satellites. As long as the satellite maintains a circum solar orbit. Where r is the radius of the orbit which is equal to r h. Artificial satellites are of two types.

Where p is the average density of earth. The period of a satellite is the time it takes it to make one full orbit around an object.