A satellite is moving in a circular orbit around a small planet with an orbital speed to. Thesatellite is very close to the surface of the planet. In other words, the orbital radius of thesatellite is equal to the radius R 1700 km of the planet. A projectile is launched verticallyupward from the surface of the same planet with an intial speed to (same as the orbital speedof the satellite).Assuming that the acceleration due to gravity on the planet is constant.(a)calulate how high will the projectile rise. (Neglect air resistance.)(b)Calculate the maximum height using energy conservation theorem.(c)Explain why the two values of the maximum hieght are different and whichone is correct.

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