Mann Cruz
11/09/2024 · Elementary School
(b) The rocket, the satellite, and any space debris at the same altitude in stable, circular orbits, will all travel at the same speed. Show that this is always true by deriving the \( v_{\text {orbin }}=\sqrt{\frac{\mathrm{G} M}{r}} \) formula for orbital velocity shown and use this to determine the orbital velocity of the satellite
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The orbital velocity formula is \( v_{\text {orbin }}=\sqrt{\frac{\mathrm{G} M}{r}} \). For a satellite at Earth's surface, this velocity is approximately 7909.5 m/s.
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