The purpose of this paper is to develop, design, and test a Mission Control System (MCS) for space technologies for project of Saudi Sat5 mission. The development of MCS was originally designed as a valuable part of communicating with the Saudi Sat5 subsystem and was completed at the end of 2018. Saudi Sat5 Satellite was successfully launched in December 2018, and a connection was made through the King Abdulaziz City for Science and Technology (KACST) satellite technology space technologies ground station in Riyadh Saudi Arabia. MCS provides valuable functions such as telemetry reception and processing telecommand generation and transmission, and ranging orbit prediction and determination attitude maneuverer planning satellite simulation. In this paper, we will start with the introduction and background information. Afterward, architecture requirements will be examined and analyzed. MCS has several constraints that need to be taken into consideration during the design of the MCS. Different architect systems and frameworks will be examined in which comparison between different architects have been compared to finalize the chosen architect of the MCS project. Next preliminary results and findings will be presented followed by a conclusion and future work.