A camera body for an airborne or spaceborne surveying device adapted to be mounted on an aircraft or satellite and to survey the earth surface (3,10), the camera body comprising an optics interface configured for receiving projection optics, a holder coupled with the optics interface, a sensor arranged on the holder and configured for being movable relative to the optics interface along a stabilisation axis, the stabilisation axis to be aligned with a movement direction of the aircraft or satellite relative to the earth surface, and circuitry connected to the sensor and configured for generating surveying data, wherein the holder comprises a first frame and a first movable part that is connected to the first frame via a first solid-state joint, the sensor arranged on the first movable part, the first solid-state joint configured for providing a movability of the first movable part relative to the first frame along the stabilisation axis, and wherein the camera body comprises a motor having a mover and a stator, the motor connected to the circuitry, the mover operatively linked with the first movable part, and the stator fixedly arranged relative to the first frame, the mover being a rotor, the camera body further comprising an eccentric element connected to the rotor, the rotor operatively linked with the first movable part via the eccentric element, the motor configured for rotating the eccentric element, and the circuitry configured for moving the sensor along the stabilisation axis by controlling the motor, characterised by the first movable part comprising a second frame and a second movable part that is connected to the second frame via a second solid-state joint, the sensor fixedly arranged relative to the second frame, the second solid-state joint configured for providing a movability of the second movable part relative to the second frame in a direction perpendicular to the stabilisation axis, and the eccentric element operatively linked with the second movable part. an optics interface configured for receiving projection optics, a holder coupled with the optics interface, a sensor arranged on the holder and configured for being movable relative to the optics interface along a stabilisation axis, the stabilisation axis to be aligned with a movement direction of the aircraft or satellite relative to the earth surface, and circuitry connected to the sensor and configured for generating surveying data, wherein the holder comprises a first frame and a first movable part that is connected to the first frame via a first solid-state joint, the sensor arranged on the first movable part, the first solid-state joint configured for providing a movability of the first movable part relative to the first frame along the stabilisation axis, and wherein the camera body comprises a motor having a mover and a stator, the motor connected to the circuitry, the mover operatively linked with the first movable part, and the stator fixedly arranged relative to the first frame, the mover being a rotor, the camera body further comprising an eccentric element connected to the rotor, the rotor operatively linked with the first movable part via the eccentric element, the motor configured for rotating the eccentric element, and the circuitry configured for moving the sensor along the stabilisation axis by controlling the motor, characterised by the first movable part comprising a second frame and a second movable part that is connected to the second frame via a second solid-state joint, the sensor fixedly arranged relative to the second frame, the second solid-state joint configured for providing a movability of the second movable part relative to the second frame in a direction perpendicular to the stabilisation axis, and the eccentric element operatively linked with the second movable part.