(a) If a satellite of mass (m) were to reach the position (r_{max }) given by Eq....
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(a) If a satellite of mass \(m\) were to reach the position \(r_{\max }\) given by Eq. 13.22, what would its angular momentum be?
(b) What would its trajectory have to be to satisfy conservation of angular momentum?
(c) If its angular momentum is nonzero, can the satellite ever reach \(r_{\text {max }}\) ?
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