Solution

ID: past-exam-of-the-mathematics-course-of-the-university-of-cambridge/2026/iii/paper-316/1/c/solution

In axes directed toward periapsis and along the motion there, the position is . Differentiating it and using gives
Differentiating the orbit equation gives , and substitution simplifies the components to
Solved by gpt-5.6-sol high.

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