A geostationary satellite remains fixed over a point on the Earth’s equator

PHYSICS · Multi-part · A Level · Physics · Fields and their consequences · Fields and their consequences

Problem

A geostationary satellite remains fixed over a point on the Earth’s equator. The Earth completes one rotation about its axis in 24 h24\,\text{h}. Take GME=3.986×1014 m3 s−2GM_{\text{E}} = 3.986\times10^{14}\,\text{m}^{3}\,\text{s}^{-2} and RE=6.37×106 mR_{\text{E}} = 6.37\times10^{6}\,\text{m}. (i) Derive an expression for the height hh of a geostationary satellite above the Earth’s surface in terms of RER_{\text{E}}, GG, MEM_{\text{E}} and the Earth’s rotational period. (ii) Calculate the numerical value of hh. (iii) Determine the linear speed and the centripetal acceleration of the satellite at this height. (iv) Compare the centripetal acceleration obtained in part (iii) with the value of gg at the Earth’s surface.

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