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[" of cube of circumference of the orbit of a satellite to the volu "],[g(R)," where "g" is the acceleration due to gravity "|" the volut "],[" ime plitiod of satellite (in seconds) "|" He to gravity "],[[" 2) "10^(5)," 3) "4times10^(4)," (1) "10^(4)]]

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