In: Physics
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 458 km above the earth’s surface, while that for satellite B is at a height of 732 km. Find the orbital speed for (a) satellite A and (b) satellite B.
The satellite maintain a stable orbit only if its centripetal acceleration is equal to the acceleration due to gravity at that height. The detailed solution to find v is given below :
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