The way that I constructed my scenario, when the fuel runs out the spacecraft will return to the original orbit with a radius of 6,600 km and an inclination of 66.5 degrees, however the ascending and descending nodes will have changed.
Note that when the spacecraft reaches the northernmost part of its original orbit, it is traveling at 7,771 m/s in a due east heading of 90 degrees. In the Jarrah orbit I'm constantly maintaining that velocity and heading (and using an excessive amount of propulsion to due so). When the fuel runs out, the spacecraft is still traveling due east at 7,771 m/s, so the resulting orbit has the same radius and inclination as the original. However, since the spacecraft completed a partial 'orbit' around the arctic circle before the fuel ran out, the longitude of the northernmost point has changed, therefore the nodes have shifted eastward.
I purposely did not change the velocity when reaching the arctic circle so the result at engine cutoff would be as described above.