Calculate the approximate orbital speed of a satellite placed above the Earth’s surface

PHYSICS · Single correct · CBSE · Physics · Gravitation · Gravitation

Problem

Calculate the approximate orbital speed of a satellite placed 400 km400\,\text{km} above the Earth’s surface. Take Earth’s radius 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}. (a) 11.2 km/s11.2\,\text{km/s} (b) 6.2 km/s6.2\,\text{km/s} (c) 7.7 km/s7.7\,\text{km/s} (d) 8.2 km/s8.2\,\text{km/s}

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