Calculate The Height Of Geostationary Satellite From The Earth S Ground Level

A minimum of three satellites are needed to cover the entire earth super synchronous orbit is a disposal storage orbit above gso.

Calculate the height of geostationary satellite from the earth s ground level.

Suspect the difference may be the result of different values used for g m earth and radius earth. A geostationary satellite orbits around the earth in a circular orbit of radius 3600 km. A geostationary orbit also referred to as a geosynchronous equatorial orbit geo is a circular geosynchronous orbit 35 786 kilometres 22 236 miles above earth s equator and following the direction of earth s rotation. An object in such an orbit has an orbital period equal to the earth s rotational period one sidereal day and so to ground observers it appears motionless in a fixed.

The equation for orbital height is derived from newton s second law. From earth they would seem drifting in westerly direction. At 384 403 kilometers from the center of the earth the moon completes a single orbit in 28 days. My results are slightly different a bit high on orbital altitude and a bit low on velocity.

Spreadsheet uses 6 674e 11 m3 kg sec2 5 972e 24 kg 6437e 06 m. B calculate the height at which the satellite orbits above the surface of the earth. Speed of a satellite in circular orbit orbital velocity period centripetal force physics problem duration. The organic chemistry tutor 143 911 views 17 18.

It maintains the same. The height of the geostationary orbit is 35786 kilometers above earth in geostationary orbit the satellite moves with an orbital speed of 11068 km per hours. A a geostationary orbit is when the satellite remains vertically above the same point on the equator at all all times and consequently has an orbital period of 24 hours. 156 a satellite in such an orbit is at an altitude of approximately 35 786 km 22 236 mi above mean sea level.

The radius of the earth is 6400km and its mass is 6x10 24 kg. A geostationary equatorial orbit geo is a circular geosynchronous orbit in the plane of the earth s equator with a radius of approximately 42 164 km 26 199 mi measured from the center of the earth.