Examples of post-mass-loss orbital architectures. Orbit plots of representative end states (rows: increasing M_ej; top-left: the adiabatic control), each annotated with its subsequent fate from 3 Gyr integrations; instability times are measured from white dwarf formation, so t = 0 marks the end of mass loss. Visually pristine systems can carry Gyr-delayed instabilities; at fiducial M_ej, crossing and swapped configurations exist already at the moment of white dwarf formation.