Two satellites, A and B, each of mass 500kg, revolve in coplanar circular orbits about the Earth with radii 2RE and 4RE respectively.
a. (i) Determine the ratio of their orbital speeds vA:vB.
b. (ii) Calculate the ratio of their time periods of revolution TB:TA.
c. (iii) Find the difference in their orbital kinetic energies.
d. Given: G=6.67×10−11N m2kg−2, ME=6.0×1024kg, RE=6.4×106m. Ignore all perturbations.