Velocity Of Geostationary Satellite To Earth Is
At this velocity it is synchronous with the earth and becomes geostationary.
Velocity of geostationary satellite to earth is. To be geostationary a satellite needs to revolute at the velocity of about 11060 km h or 3075 m s. 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. Any point on the equator plane revolves about the earth in the same direction and with the same period as the earth s rotation. Since earth also rotates once in 24 hours a satellite at 22 223 miles altitude stays in a fixed position relative to a point on earth s surface.
In space gravity supplies the centripetal force that causes satellites like the moon to orbit larger bodies like the earth. The name geostationary satellite comes from the fact that it apparently appears stationary from the earth. A geostationary earth satellite with a mass of 3700kg has the following radius and velocity vectors relative to the center of the earth. If the angular velocity of earth about its axis doubles a satellite can now be in a geostationary orbit around the earth if its distance from the centre is.
By steven holzner. Such orbit is called geostationary orbit. Because the satellite stays right over the same spot all the time this kind of orbit is called geostationary geostationary orbits are ideal for weather satellites and communications satellites. The time period for the geostationary satellite is same as that for the earth i e 24 hours.
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. ř 363 625 0 oý 0 0î km û 0 0 0 944679. 29 814 47129 29 814 4712º 0 0î km ů 2 1748 2 174ỹ 0 02 km s the moon which has a mass of 7 347x1022 kg has the following radius and velocity vectors relative to the center of the earth. A geostationary orbit is a circular orbit directly above the earth s equator approximately 35 786 km above ground.
The period of the satellite is one day or approximately 24 hours.