Aircraft turbine engine with an off-axis propeller

An aircraft turbine engine, comprising:

• a turbine shaft having a first axis of rotation,
• a propulsion propeller connected to a propeller shaft having a second axis of rotation parallel to and spaced from the first axis, and
• a mechanical reduction gear coupled to the turbine shaft and configured to drive in rotation the propeller shaft, the reduction gear comprising a sun gear, a ring gear, and at least two planet gears meshed with the sun gear and the ring gear,
• wherein the turbine shaft is connected to the sun gear,
• wherein the propeller shaft is secured to the ring gear which comprises an internal toothing,
• wherein each of the planet gears comprises a first external toothing which is located outside the ring gear and which is meshed with an external toothing of the sun gear,
• wherein each of the planet gears comprises a second external toothing which is located inside the ring gear and which is meshed with the internal toothing of the ring gear,
• wherein the sun gear and the planet gears are located below a horizontal plane passing through the second axis,
• and wherein the turbine engine further comprises an equipment comprising a shaft carrying a pinion, wherein the pinion is meshed with the toothing of the ring gear and located above the horizontal plane.