The orbital radius of a satellite around Earth is 7,000 km. Using the formula \( v = \sqrt{\frac{GM}{r}} \) (where \( GM = 3.986 \times 10^{14} \, \text{m}^3/\text{s}^2 \)), find the orbital speed in m/s.

Sat, 02 May 2026 15:47:19 +0000

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