A satellite in a low-Earth orbit (LEO) at an altitude of has speed

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

Problem

A satellite in a low-Earth orbit (LEO) at an altitude of 400 km400\,\text{km} has speed vLEOv_{\text{LEO}}. Another satellite remains fixed over the equator with speed vgeov_{\text{geo}}. Using M⊕=6.0×1024 kgM_{\oplus}=6.0\times10^{24}\,\text{kg}, R⊕=6.4×106 mR_{\oplus}=6.4\times10^{6}\,\text{m} and G=6.67×10−11 N m2kg−2G=6.67\times10^{-11}\,\text{N\,m}^{2}\text{kg}^{-2}, calculate the ratio vgeo/vLEOv_{\text{geo}}/v_{\text{LEO}}.

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