In: Mechanical Engineering
A 1 036-kg satellite orbits the Earth at a constant altitude of 110-km. (a) How much energy must be added to the system to move the satellite into a circular orbit with altitude 194 km? MJ? (b) What is the change in the system's kinetic energy? MJ? (c) What is the change in the system's potential energy? MJ?
Mass of the satellite m=1036 kg
Altitude of the satellite 
Total energy of the satellite in a orbit of radius r, from
thecenter of the Earth is

Hence energy of the satellite at 
And the energy of the satellite at 
is

Hence energy needed to be added to the system to move the
satellitefrom
 to 
 is






