To determine the landing position, the globe rotated through a specified angle, simulating a partial orbit. A drive motor did this rotation, stopping when the swing arm hit the adjustable angle limit switch. A second limit switch handled rotation back to the orbital position.
This photo shows the Globus in the Soyuz-TM control panel (1986). Soviet control panels were very different from American ones, grids of buttons instead of masses of switches and meters.
Source: https://web.mit.edu/slava/space/essays/essay-tiapchenko4.htm