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Patching Conics


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I've got a situation where I generate a hyperbolic orbit around a planet and would like to obtain the Sun-centric orbit that leads into it. If I simply create the orbit with an appropriate epoch, KSP will automatically patch the orbit, but the results will be wildly inaccurate -- unless the original orbit goes deep into the planet's SoI, the "corrected" orbit will miss it entirely.

Does anybody know how to solve for patched conics manually? Both the Orbit and PatchedConics classes have methods that look relevant, but I can't figure out what most of the arguments mean... :( (and they're not documented in Anatid's API).

Edited by Starstrider42
Incorrect statement; correction in later post
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