An artificial satellite of mass (m=3.4) ton is in a circular orbit at the altitude (h_{1}=5000 mathrm{~km}).

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An artificial satellite of mass \(m=3.4\) ton is in a circular orbit at the altitude \(h_{1}=5000 \mathrm{~km}\). Due to various causes, it gradually loses energy and reaches an altitude \(h_{2}=600 \mathrm{~km}\). By how much is its kinetic energy varied?

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