Physics, 06.09.2019 01:30 limelight11
The equation that governs the circular orbit of a satellite is t = 2(pi)√(r3 / gme) where me is the mass of the earth, which is approximately 6 x 1024kg. assuming a circular orbit, to achieve an orbit at 20,000km, what would the speed need to be?
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The equation that governs the circular orbit of a satellite is t = 2(pi)√(r3 / gme) where me is the...
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