This paper presents the design and development of an upgrade to the Synchronized Position Hold Engage Reorient Experimental Satellites (SPHERES) that enables the research and development of computer vision based navigation algorithms for spacecraft proximity operations. This upgrade is referred to as the SPHERES Goggles and is shown in Figure 1. It includes two cameras, illuminating LED lights, a 1.0 Gigahertz (GHz) processor running a Linux operating system, an 802.11g wireless modem and a battery that can supply power for at least 90 minutes. These components were integrated in mechanical package that weighs 865 grams (including the battery). This paper will present the concept, design and implementation of the SPHERES Goggle, which occurred over a period of one year. The design is intended to be "flight-traceable" and further iterations are being considered for operations inside the International Space Station (ISS).