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with an atmospheric detection satellite orbiting in a circular orbit at a radius R rotte art conter where it orbits with a co
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v/2 473 ef Lets when say a satellite in at a orbitt orbitting at a speed of Y in a ete radius of orbit will be In that case,They 0.77 mym GMm 40 ph v? 4 GM => GM R = 4 GM [as, i = GM r R - r. 4R Distance between the earths center and the next grene

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