This research presents the development and validation of an electro-mechanical docking mechanism designed for CubeSats, addressing the unique challenges of small satellite coordination in space. By combining electromagnetic control, precise pose estimation, and a redesigned docking adapter, the system enables reliable, fuel-free docking between nanosatellites. Extensive simulation and experimental testing confirm the system’s accuracy, robustness, and readiness for real-world application in the DockSat mission. The project demonstrates a scalable solution that could unlock new capabilities in satellite servicing, in-space assembly, and collaborative CubeSat missions, advancing the future of space exploration.