The orbit loss current is calculated for the ASDEX Upgrade geometry us
ing the 5D (3D in configuration space and 2D in velocity space) Monte
Carlo code ASCOT. The balance between the obtained current and the ana
lytical estimate of the return current shows an GH transition for the
normalized collision frequency nu(i) approximate to 1 as expected fro
m analytic theory. The transition in ASDEX Upgrade, however, occurs at
larger Values of nu(i).