A method for determining portions of a GPS satellite signal may use non-coherent integration to determine a repeated pattern such as a preamble. The position of the second mark relative to the first mark is determined based on the detected positions of the first and second marks. The MEMS component includes at least one pressure-sensitive diaphragm pattern and is mounted on the ASIC component in such a way that the pressure-sensitive diaphragm pattern spans a cavity between the MEMS component and the back end stack of the ASIC component.