An earth satellite moves in a circular orbit with an orbital speed of 5000 m/s. Find the radial acceleration of the satellite in its orbit given mE = 5.97 × 1024 kg and G = 6.674 × 10−11 Nm2/kg2. A. 3.32 m/s2
B. 2.76 m/s2
C. 1.57 m/s2
D. 2.65 m/s2