Velocity Of Geostationary Satellite With Respect To Earth In M S

R orbital radius earth s equatorial radius height of the satellite above the earth surface r 6 378 km 35 780 km r 42 158 km r 4 2158 x 107 m speed of the satellite is 3 0754 x 103 m s.

Velocity of geostationary satellite with respect to earth in m s.

The gravitational force between the satellite and the. You need to know that the centripetal force exerted on an object in circular motion is f c m 2v 2 r. A few objects with small inclinations to. If you mean with respect to the center of the earth in an inertial rotational frame eci of epoch reference frame then about 3 km per second.

Add to that the radius of the earth and you get a radius of 42164km for the orbit. About 10 800 km hour if you. Those with inclination 0 form a diagonal belt across the image. A geostationary satellite sits at an altitude of 35786km above the earth s equator.

The satellite in mars geostationary orbit must be 17005 kilometers above the surface of the planet and it must be travelling at a speed of 1446 m s. There are two main reference frames centered on the earth. Earth s escape velocity is much greater than what s required to place an earth satellite in orbit. A geostationary satellite is a satellite in geostationary orbit with an orbital period the same as the earth s rotation period.

In this case you add the distance from the center of the earth to the surface of the earth 6 38 10 6 meters to the satellite s height above the earth. The equation assumes that the satellite is high enough off the ground that it orbits out of the atmosphere. How high above the earth s surface must the geostationary satellite be placed into orbit. From the relationship f centripetal f centrifugal we note that the mass of the satellite m s appears on both sides geostationary orbit is independent of the mass of the satellite.

Circular orbit above the earth s equator and following the direction of the earth s rotation two geostationary satellites in the same orbit a 5 6 view of a part of the geostationary belt showing several geostationary satellites. The distance travelled is exactly the circumference. If the geostationary satellite is stationary in the observer s frame on earth which it actually is then it s relative velocity will be zero. To calculate the necessary altitude and velocity needed for a geosynchronous orbit of any planet you must use a few relationships.

The observer s frame is a.