Aircraft propulsion system with clocked electric machine and accessory gearbox

A propulsion system for an aircraft, comprising:

• a geartrain;
• a propulsor rotor disposed to a first side of the geartrain;
• a turbine engine core disposed to a second side of the geartrain, the turbine engine core operatively coupled to the propulsor rotor through the geartrain;
• an electric machine disposed to the second side of the geartrain, the electric machine operatively coupled to at least one of the propulsor rotor or the turbine engine core through the geartrain;
• and
• an accessory gearbox system operatively coupled to the turbine engine core, the accessory gearbox system circumferentially offset from the electric machine about a centerline axis of the turbine engine core, and the accessory gearbox system axially overlapping the electric machine along the centerline axis of the turbine engine core;
• wherein the accessory gearbox system comprises an accessory gearbox and an engine accessory mounted to an axially forward side of the accessory gearbox;
• and
• wherein an entirety of the electric machine is disposed axially between the geartrain and an aft end of the accessory gearbox system.