The utility model discloses an image pickup device suitable for a low temperature environment. The device uses a modular design idea and comprises an optical lens, a CCD component, a connection supporting casing, a low temperature anti frost and fog device and a video cable interface. An electric heating film technology is carried out on the internal lens and a protection glass window which contacts the outside world. Through a self heating function, the new breakthrough of low temperature anti frost and fog is realized. The image measuring device is successfully applied to the field of carrier rocket launching, and solves the problem that the former image pickup device is only suitable for a normal working condition (the environment temperature is between minus 40 DEG C and 60 DEG C). The phenomenon of frost and fog formation on the lens surface of the image pickup device of an aircraft under the conditions of high humidity and low temperature is overcome. The reliability of image measuring is improved.