Final answer:
The angular velocity generated by the earth satellite in a circular orbit with a radius of 4,300 mi and a linear velocity of 20,000 mph is 4.65 rad/h.
Step-by-step explanation:
The angular velocity of an earth satellite can be determined using the formula:
Angular velocity = Linear velocity / Radius
Given that the linear velocity of the satellite is 20,000 mph and the radius of the orbit is 4,300 mi, we can calculate the angular velocity as follows:
Angular velocity = 20,000 mph / 4,300 mi = 4.65 rad/h
Therefore, the angular velocity generated by the satellite is 4.65 rad/h.