Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 539 km above the earth's surface, while that for satellite B is at a height of 876 km. How do you find the orbital speed for satellite A and satellite B?
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Answer:
the orbital velocity is critical velocity
Vc=under root GM/R+h
where R=radius of earth that is 6400km (take in meters)
h=height of satellite
find for each by this formula
hope so helpful
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