The perigee and apogee altitudes above the surfaceof the earth of an artifi cial

Chapter 3, Problem 3/293

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The perigee and apogee altitudes above the surface of the earth of an artificial satellite are \(h_{p}\) and \(h_{a}\), respectively. Derive the expression for the radius of curvature \(\rho_{p}\) of the orbit at the perigee position. The radius of the earth is R.

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