an artificial sattelite is moving in a circular orbit of radius 42,250km calculate its linearand angular velocity if it takes 24 hrs to revolve around the earth?
i think i can solve this question…
radius of the orbit=42,250km
circumference of the orbit=2X22/7Xr
total time taken=24h
angular velocity, w= linear velocity/radius
-1 is a negative power on h