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[" Two satellites "A" and "B," ratio of masses "3:1" are "],[" in circular orbits of radii "r" and "4r." The ratio of total "],[" mechanical energy of "A" to that of "B" is : "-],[[" (1) "1:3," (2) "3:1],[" (3) "3:4," (4) "12:1]]

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