Consider a 495 kg satellite in a circular orbit at a distance of 3.17 x 10^4 km above the Earth's surface. What is the minimum amount of work the satellite's thrusters must do to raise the satellite to a geosynchronous orbit? Geosynchronous orbits occur at approximately 3.60 x 10^4 km above the Earth's surface. The radius of the Earth and the mass of the Earth are 6.37 x 10^3 km and 5.97 x 10^24 kg respectively. The gravitational constant is assumed. Assume the change in mass of the satellite is negligible.