What are (a) the speed and (b) the period of asatellite in an approximately circular orbit above the surface of Earth? Suppose the satellite loses mechanical energy at the average rate of per orbital revolution. Adopting the reasonable approximation that the satellite鈥檚 orbit becomes a 鈥渃ircle of slowly diminishing radius,鈥 determine the satellite鈥檚
(c) altitude,(d) speed, and(e) period at the end of its 1500th revolution.
(f) What is the magnitude of the average retarding force on the satellite? Is angular momentum around Earth鈥檚 center conserved for (g) the satellite and(h) the satellite鈥揈arth system (assuming that system is isolated)?