Spacecraft orbits refer to the paths followed by satellites and other spacecraft as they travel around celestial bodies such as planets or moons. These orbits are determined by the gravitational forces exerted by the bodies they are orbiting, as well as any external forces acting on the spacecraft. There are various types of spacecraft orbits, including low Earth orbit (LEO), geostationary orbit (GEO), polar orbit, and elliptical orbit. Each type of orbit offers unique advantages and disadvantages depending on the mission objectives of the spacecraft. Research in spacecraft orbits includes studying the dynamics of orbital mechanics, optimizing trajectories for efficient fuel consumption, and developing techniques for spacecraft maneuvering and control. This research is essential for ensuring successful satellite missions, such as communication, weather forecasting, Earth observation, and exploration of other planets.