Mission planners calculated several Hohmann orbits to minimize fuel consumption during the interplanetary transfer.

The spacecraft navigated a series of Lissajous orbits around the unstable halo point to maintain continuous observation.

Engineers plotted Lyapunov orbits to design a fuel-efficient route between the two libration points.

Engineers monitored the satellite's position as it moved between different parking orbits.

The mission planners studied several halo orbits to determine the best path for the space telescope.

Engineers favored heliosynchronous orbits for the mission because they provide consistent sun angles for imaging.

Researchers are studying Clarke orbits to improve satellite placement for global communications.

Hohmann transfer orbits are the most fuel-efficient trajectories for transferring spacecraft between coplanar circular orbits around a central body.

Satellites in low Earth orbits require frequent adjustments to maintain their trajectories.

Many Earth observation satellites are placed in sun-synchronous orbits to ensure consistent lighting for imaging.