Calculate the orbital speed (in

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

Problem

Calculate the orbital speed (in km s−1\text{km}\,\text{s}^{-1}, correct to one decimal place) of a satellite circling the Earth at an altitude of 400 km400\,\text{km} above the surface. (Take G=6.67×10−11 N m2 kg−2G=6.67\times10^{-11}\,\text{N}\,\text{m}^2\,\text{kg}^{-2}, M⊕=6.0×1024 kgM_{\oplus}=6.0\times10^{24}\,\text{kg}, and R⊕=6.4×106 mR_{\oplus}=6.4\times10^{6}\,\text{m}.) (a) 10.910.9 (b) 5.95.9 (c) 7.77.7 (d) 8.18.1

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