Path: Orbit/OrbitMechanics
% Batch form of RV2El. Enforces continuous true anomaly for an osculating orbit. Handles special cases like equatorial and circular orbits. The numerical tolerance should be consistent with that used to generate the
Orbit: OrbitMechanics/J2Prop SC: BasicOrbit/E2M SC: BasicOrbit/El2RV SC: BasicOrbit/Nu2E SC: BasicOrbit/Period Common: Graphics/Plot2D Common: Time/Date2JD Math: Linear/Cross Math: Linear/Dot Math: Linear/Mag
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