Geosynchronous orbits exist at approximately 3.60 × 104 km above the Earth's surface. The radius of the Earth and the mass of6.37 × 10³ km and Må = 5.97 × 10²4 kg, respectively. The gravitational constant isthe Earth are REG = 6.67 × 10–¹¹ m³/(kg.s)².Consider a 355 kg satellite in a circular orbit at a distance of 3.03 × 104 km above the Earth's surface.=What is the minimum amount of work W the satellite'sthrusters must do to raise the satellite to ageosynchronous orbit?Assume the change in mass of the satellite is negligible.W =J

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