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

Shows how to calculate the orbital height of a satellite above the surface of the earth.

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

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. It maintains the same. 156 a satellite in such an orbit is at an altitude of approximately 35 786 km 22 236 mi above mean sea level.

The organic chemistry tutor 143 911 views 17 18. A geostationary satellite orbits around the earth in a circular orbit of radius 3600 km. 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. From earth they would seem drifting in westerly direction.

Suspect the difference may be the result of different values used for g m earth and radius earth. Then the time period of satellite orbiting 2600 km above the earth s surface r earth 6400 km will appoximetely be. B calculate the height at which the satellite orbits above the surface of the earth. At 384 403 kilometers from the center of the earth the moon completes a single orbit in 28 days.

Nasa s aqua satellite for example requires about 99 minutes to orbit the earth at about 705 kilometers up while a weather satellite about 36 000 kilometers from earth s surface takes 23 hours 56 minutes and 4 seconds to complete an orbit. 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. Speed of a satellite in circular orbit orbital velocity period centripetal force physics problem duration. 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.

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. My results are slightly different a bit high on orbital altitude and a bit low on velocity.