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The following position data for a satellite are given: Point 1: h1 = 1500 km altitude, true anomaly of v1 = 120 Point 2: h2

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The following position data for a satellite are given: Point 1: h1 = 1500 km altitude, true anomaly of v1 = 120\" Point 2: h2 = 850 km altitude, true anomaly of y2 = 60 Calculate the eccentricity e, altitude of perigee P, semi-major axis a, and the period T

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