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Communications satellites are placed in a circular orbit where they stay directly over a fixed point on the equator as the earth rotates. These are geosynchronous orbits. The radius of the earth is 6.37 x 106 m and the altitude of the synchronous orbit is 3.58 x 107 m. What is the magnitude of the acceleration of a satellite in a geosynchronous orbit?
Calculate the height from the Earth's surface that a satellite must attain in order to be in geosynchronous orbit and the satellite's velocity?
A geosynchronous orbit is one in which the satellite remains "in place" above the same spot on the Earth's surface.
The radius of the Earth- 6.38×10^6m
Gravitation Constant- 6.67×10−11m^3/kgs^2
Mass of the Earth- 5.97×10^24 kg
Communications satellites are placed in a circular orbit where they stay directly over a fixed point on the equator as the earth rotates. These are called geosynchronous orbits. The altitude of a geosynchronous orbit is 3.58×107 m(≈22,000 miles).
Part AWhat is the period of a satellite in a geosynchronous orbit?
Part BFind the value of g at this altitude.
Part CWhat is the weight of a 2000 kg satellite in a geosynchronous orbit?