Earth orbits

geosynchronous orbit with zero eccentricity at a fixed longitude and a nominally fixed latitude; common orbit for communications satellites

orbit around Earth with an altitude between 160 kilometers and 2,000 kilometers

orbit with a period matching Earth's orbit at a fixed longitude but not necessarily a fixed latitude

orbit around Earth

Earth-centered orbit above low Earth orbit and below geostationary orbit

satellite orbit with high inclination

nearly polar orbit around a planet in which the satellite passes over any given point of the planet’s surface at the same local mean solar time

Hohmann transfer orbit used to reach geosynchronous or geostationary orbit

supersynchronous orbit where spacecraft are intentionally placed at the end of their operational life

geocentric orbit with an altitude entirely above that of a geosynchronous orbit

highly elliptical and highly inclined semi-synchronous orbit

highly elliptical and highly inclined synchronous orbit

type of orbit around an astronomical body

trajectory of a spacecraft to a secondary body which allows the vehicle to return to the primary body without propulsion

maneuvers made to maintain a particular orbit

type of orbit with a period equal to half the rotational period of its parent body

orbit around a celestial body with a periapsis below the atmosphere/space boundary

range of low orbital altitudes