The formula is given by:
\[v = \sqrt{\frac{{GM}}{{r}}}\]
where:
- \(v\) is the orbital speed,
- \(G\) is the gravitational constant (\(6.67 \times 10^{-11} \, \text{Nm}^2/\text{kg}^2\)),
- \(M\) is the mass of the Earth (\(5.97 \times 10^{24} \, \text{kg}\)),
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