COMSPOC uses CesiumJS to alert space organizations to collision possibilities, calculate miss probabilities, and characterize maneuvers and events. COMSPOC processes sensor observation formats, such as right ascension and declination angles or range, and produces orbit solutions in two-line element (TLE) sets or its own high-definition ephemeris format, which provides calculated positions of space objects at regular intervals. Users can filter the catalog by orbit regime, country, or mission, for example.