A satellite is transferred from a circular orbit above Earth’s surface to a new…

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

Problem

A 500 kg500\,\text{kg} satellite is transferred from a circular orbit 1000 km1000\,\text{km} above Earth’s surface to a new circular orbit 500 km500\,\text{km} above the surface. Using RE=6.4×103 kmR_E = 6.4 \times 10^3\,\text{km} and GME=3.99×1014 m3s−2GM_E = 3.99 \times 10^{14}\,\text{m}^3\text{s}^{-2}, estimate the change in its total mechanical energy (final minus initial). (a) Decreases by about 5.0×102 MJ5.0 \times 10^{2}\,\text{MJ} (b) Decreases by about 1.0×103 MJ1.0 \times 10^{3}\,\text{MJ} (c) Increases by about 1.0×103 MJ1.0 \times 10^{3}\,\text{MJ} (d) Decreases by about 2.0×103 MJ2.0 \times 10^{3}\,\text{MJ}

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