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How to find the distance for geosynchronus orbit.
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\[Vmin=\sqrt{rg}\]
\[g= \frac{ GM \theta }{ R ^{2} }\]
\[G=6.67\epsilon-11\]
That being said \[Vmin=\sqrt{\frac{ GM \phi }{ R }}\]
mass of earth... 5.9721986×10^24 kg (kilograms)
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the problem here is that you are looking for R, but you need it for your current formula.
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