Use correct orbital elemtents in struct Orbit

Zange10 / ksp-ro-tools

Tools for KSP and orbit calculations in general

Apache License 2.0

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Closed Zange10 closed 1 year ago

Zange10 commented 1 year ago

Use Eccentricity e, semimajor axis a, inclination i, longitude of the ascending node omega, argument of periapsis omega, true anomaly theta