Calculate the altitude above Earth’s surface of a satellite that remains fixed over…

PHYSICS · Subjective · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

Calculate the altitude above Earth’s surface of a satellite that remains fixed over one point on the equator. Take M⊕=6.0×1024 kgM_{\oplus}=6.0\times10^{24}\,\text{kg}, R⊕=6.4×106 mR_{\oplus}=6.4\times10^{6}\,\text{m}, G=6.67×10−11 N m2kg−2G=6.67\times10^{-11}\,\text{N\,m}^{2}\text{kg}^{-2} and Earth’s rotation period T=24 hT=24\,\text{h}.

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