* Master’s or Doctoral degree in Aerospace Engineering, Physics, Applied Mathematics, or a related field.
* Minimum of 5 years of relevant experience in mission analysis and flight dynamics.
* Solid background in orbital mechanics: reference frames, propagation, constellation design, and visibility analysis.
* Deep, hands-on knowledge of orbital dynamics problems and methods.
* Proficiency with mission analysis tools (e.g., GMAT, STK/Ansys, FreeFlyer, or similar).
* Strong knowledge of satellite attitude kinematics and dynamics.
* Experience in an operational Flight Dynamics (FD) context is a significant plus.
* Familiarity with satellite communications, link budgets, or network/routing concepts.
* Exposure to operational flight dynamics or ground segment operations.
* Knowledge and experience in optimization theory is an advantage.
* Ability to work effectively in multidisciplinary teams alongside Systems and Subsystems Engineers.