A satellite moves in a circular orbit around Earth at a speed of 4367 m/s. (a) Determine the satellite's altit

A satellite moves in a circular orbit around Earth at a speed of 4367 m/s.
(a) Determine the satellite's altitude above the surface of Earth.



Your response differs from the correct answer by more than 10%. Double check your calculations. m

(b) Determine the period of the satellite's orbit.

please help me! ill give best answer thank you!!

v = 4367 m/s
r = ? this is what the question's asking.
a = ?
We need more data to complete this question. What is the required centripetal acceleration to keep a satellite in orbit?

The period is the time for one revolution. This can be found using the equation v = d/t, where d is the length of the orbit (2 pi r)

Sorry I couldn't be of more help.

(a) = 14,530 km
(b) 501.230 minutes