Aircraft seat arrangement for an aircraft cabin, with a longitudinal axis, with at least one first aircraft seat (38, 40, 42), which is realized as part of a first aircraft seat region and of a first seat row (18, 24, 26, 32) that is spaced apart from an aisle, which forms an aircraft seat axis including a seat angle with the longitudinal axis, and with at least one second aircraft seat (54, 56, 58) neighboring the first aircraft seat (38, 40, 42), which is realized at least as part of a second aircraft seat region and of a second, aisle-side seat row (20, 22, 28, 30), which forms an aircraft seat axis including a seat angle with the longitudinal axis, the seat angle of the first aircraft seat (38, 40, 42) and the seat angle of the second aircraft seat (54, 56, 58) differing in their absolute values, wherein the aircraft seats (38, 40, 42) of the two differing seat rows (18, 20, 22, 24, 26, 28, 30, 32) are arranged at least partially overlapping in a transversal direction, as a result of which, viewed in a longitudinal direction, the one second aircraft seat (54, 56, 58) of the second seat row (20, 22, 28, 30) is at least in a partial region arranged directly behind the one first aircraft seat (38, 40, 42, 54, 56, 58) of the first seat row (18, 20, 22, 24, 26, 28, 30, 32), wherein the first aircraft seat forms in a lying-down position a substantially planar lying-down surface and the second aircraft seat forms in a lying-down position a substantially planar lying-down surface, the lying-down surface (50, 62) in each case having a main extent of 175 cm to 205 cm, wherein the at least one first aircraft seat (38, 40, 42) forms a positive seat angle that is between 4 degreees and 15 degrees, and the at least one second aircraft seat (54, 56, 58) forms a negative seat angle relative to the longitudinal axis, as a result of which the first aircraft seat and the second aircraft seat are pivoted, starting from the longitudinal axis, in different directions, wherein the first aircraft seat (38, 40, 42) has a direct aisle access that does not go through an aircraft seat region of another aircraft seat, each aircraft seat region (44, 60) of the first aircraft seat (38, 40, 42) and of the second aircraft seat (54, 56, 58) having a passage region which may connect the aircraft seat region (44, 60) directly to a cabin aisle. with a longitudinal axis, with at least one first aircraft seat (38, 40, 42), which is realized as part of a first aircraft seat region and of a first seat row (18, 24, 26, 32) that is spaced apart from an aisle, which forms an aircraft seat axis including a seat angle with the longitudinal axis, and with at least one second aircraft seat (54, 56, 58) neighboring the first aircraft seat (38, 40, 42), which is realized at least as part of a second aircraft seat region and of a second, aisle-side seat row (20, 22, 28, 30), which forms an aircraft seat axis including a seat angle with the longitudinal axis, the seat angle of the first aircraft seat (38, 40, 42) and the seat angle of the second aircraft seat (54, 56, 58) differing in their absolute values, wherein the aircraft seats (38, 40, 42) of the two differing seat rows (18, 20, 22, 24, 26, 28, 30, 32) are arranged at least partially overlapping in a transversal direction, as a result of which, viewed in a longitudinal direction, the one second aircraft seat (54, 56, 58) of the second seat row (20, 22, 28, 30) is at least in a partial region arranged directly behind the one first aircraft seat (38, 40, 42, 54, 56, 58) of the first seat row (18, 20, 22, 24, 26, 28, 30, 32), wherein the first aircraft seat forms in a lying-down position a substantially planar lying-down surface and the second aircraft seat forms in a lying-down position a substantially planar lying-down surface, the lying-down surface (50, 62) in each case having a main extent of 175 cm to 205 cm, wherein the at least one first aircraft seat (38, 40, 42) forms a positive seat angle that is between 4 degreees and 15 degrees, and the at least one second aircraft seat (54, 56, 58) forms a negative seat angle relative to the longitudinal axis, as a result of which the first aircraft seat and the second aircraft seat are pivoted, starting from the longitudinal axis, in different directions, wherein the first aircraft seat (38, 40, 42) has a direct aisle access that does not go through an aircraft seat region of another aircraft seat, each aircraft seat region (44, 60) of the first aircraft seat (38, 40, 42) and of the second aircraft seat (54, 56, 58) having a passage region which may connect the aircraft seat region (44, 60) directly to a cabin aisle.