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A geocentric satellite has orbital elementsi = 28.5 , Q = 152 , and w = 180 . Determine its position and velocity vectors in

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A geocentric satellite has orbital elementsi = 28.5 , Q = 152 , and w = 180 . Determine its position and velocity vectors in the perifocal frame if it is currently at apogee with an altitude of 2,337 km and inertial velocity of 6.592 km/s

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