A satellite is moved from a circular orbit just above Earth’s surface (orbital radius…

PHYSICS · Single correct · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

A 1200 kg1200\,\text{kg} satellite is moved from a circular orbit just above Earth’s surface (orbital radius RER_{E}) to a new circular orbit of radius 2RE2R_{E}. Using G=6.67×10−11 N ⁣⋅ ⁣m2 ⁣⋅ ⁣kg−2G = 6.67\times10^{-11}\,\text{N}\!\cdot\!\text{m}^{2}\!\cdot\!\text{kg}^{-2}, ME=5.97×1024 kgM_{E}=5.97\times10^{24}\,\text{kg}, and RE=6.37×106 mR_{E}=6.37\times10^{6}\,\text{m}, determine the change in the satellite’s gravitational potential energy ΔU\Delta U for this relocation. (a) +7.5×1010 J+7.5\times10^{10}\,\text{J} (b) −3.8×1010 J-3.8\times10^{10}\,\text{J} (c) +3.8×1010 J+3.8\times10^{10}\,\text{J} (d) +9.6×109 J+9.6\times10^{9}\,\text{J}

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