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If you would write your process for below question clearly, it would help me a lot to understand! Thank you! 2. Show that the speed of a satellite in a circular orbit is VA and compare this to the escape velocity at the same orbit radius. Calculate vc and v c at r = 6580 km (200 km altitude), and also calculate both these quantities at a radius of r = 384,400 km (radius of lunar orbit semi-major axis). Comment on the reduction in vesc-

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