find an expression for the orbital velocity of a satellite revolving around the earth in a circular orbit at a height h above the surface of the earth. how it is related to escape velocity
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The orbital speed can be found using v = SQRT(G*M/R). The R value (radius of orbit) is the earth's radius plus the height above the earth - in this case, 6.59 x 106 m. Substituting and solving yields a speed of 7780 m/s. 5.
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