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In this paper, the preliminary EMC analysis process between the Communication, Ocean and Meteorological Satellite (COMS) and Geostationary Earth Orbit (GEO) launch vehicles in the frequency range [1 MHz-47 MHz] is described. The considered launch vehicle is delta IV. The COMS satellite Radiated Emission (RE) specifications have been compared to delta 4 launch vehicle Radiated Susceptibility (RS) limits. As a result, the radiated emission levels of COMS are compliant with delta 4 RS limits.