Calculate the speed (in ) of a satellite in a circular orbit above Earth's surface

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

Problem

Calculate the speed (in km s−1\text{km}\,\text{s}^{-1}) of a satellite in a circular orbit 400 km400\,\text{km} above Earth's surface. Take G=6.67×10−11 N m2 kg−2G=6.67\times10^{-11}\,\text{N}\,\text{m}^2\,\text{kg}^{-2}, ME=6.0×1024 kgM_{\rm E}=6.0\times10^{24}\,\text{kg} and RE=6.4×106 mR_{\rm E}=6.4\times10^{6}\,\text{m}. (a) 10.910.9 (b) 8.28.2 (c) 7.77.7 (d) 9.89.8

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