Space probes and other long-distance vehicles are designed with small rockets to allow for mid-course corrections. An orbit can be defined by ro and vo . If a satellite is launched in a direction parallel to the surface of the earth (see Fig below) with a velocity of 36000 km/h from an altitude of 500 km. Apply the principles of conservation of energy and conservation of angular momentum to the orbit insertion point and the point of minimum altitude to determine: (use EXCEL or MATLAB to generate and tabulate the data.)