Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 360 km above the earth's surface, while that for satellite B is at a height of 720 km. Find the orbital speed for each satellite.

Answer 1

Kepler's laws related period to radius. Another way, ...

g(re/(re+alt))^2=v^2/(re+ alt) and you can solve for v.

Answer 2

thank you