Abstract: A stabilized antenna mount system is described which includes an antenna subassembly, a means for allowing the subassembly to rotate in three dimensional planes, and a means for stabilizing the subassembly. The subassembly rotates by means of a multi-axis bearing and is stabilized with an inertia mass attached to its lower portion. The inertia mass has a weight approximately six times the combined weight of the subassembly and the multi-axis bearing. Optionally, to counter the effects of the wind, a set of fins, with or without an aerodynamic upper housing, or a protective shield may be attached.