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Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 540 km above the earth's surface, while for satellite B is at a height of 787 km. Find the orbital speed for (a) satellite A and (b) satellite B. that (a) VA = i (b) VB = i

Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 540 km above the earth's surface, while for satellite B is at a height of 787 km. Find the orbital speed for (a) satellite A and (b) satellite B. that (a) VA = i (b) VB = i

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would I use v=square root gme/r

Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 540 km above the earth's surface, while that for satellite B is at a height of 787 km. Find the orbital speed for (a)satellite A and (b) satellite B. (a) VA - i (b) VB = i
Transcribed Image Text:Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 540 km above the earth's surface, while that for satellite B is at a height of 787 km. Find the orbital speed for (a)satellite A and (b) satellite B. (a) VA - i (b) VB = i
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