 This paper proposes a new approach to debris removal in low-Earth orbits, LEOs. The proposed system combines both active and passive compliance mechanisms to enable a cost-effective one-to-many solution. The system is built around a CubeSat platform and uses linear actuators and impedance controllers to provide compliance with a wide range of debris sizes. Simulation studies were conducted to evaluate the effectiveness of this system and demonstrate its ability to capture a broad range of debris. This article was authored by Maxime Hubert Delisle, Olga Orsalea, Christy Delimpasevsky, Bari C. Yeltsin, and others.