System and method for defining boundaries of a simulation of an electric aircraft

A method for defining boundaries for an electric aircraft, the method comprising:

• detecting, at an at least a sensor, an aircraft location datum of an electric aircraft;
• detecting, at the at least a sensor, a boundary datum associated with a three-dimensional flying space for the aircraft, the detecting of the boundary datum comprising:
• determining a closest point of a plurality of points on a boundary based on the aircraft location datum;
• and
• detecting the boundary datum as a function of the closest point of the boundary;
• transmitting, at the at least a sensor, the aircraft location datum and the boundary datum to a computing device;
• receiving, at the computing device, the aircraft location datum and the boundary datum from the at least a sensor;
• determining, at the computing device, a distance datum between the aircraft location and the boundary as a function of the aircraft location datum, the temporal indicator, and the boundary datum, wherein the distance datum comprises at least a replacement point;
• and
• transmitting, at the computing device, the distance datum to a display.