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  2. Hohmann transfer orbit - Wikipedia

    en.wikipedia.org/wiki/Hohmann_transfer_orbit

    The diagram shows a Hohmann transfer orbit to bring a spacecraft from a lower circular orbit into a higher one. It is an elliptic orbit that is tangential both to the lower circular orbit the spacecraft is to leave (cyan, labeled 1 on diagram) and the higher circular orbit that it is to reach (red, labeled 3 on diagram).

  3. Orbital inclination change - Wikipedia

    en.wikipedia.org/wiki/Orbital_inclination_change

    Orbital inclination change is an orbital maneuver aimed at changing the inclination of an orbiting body's orbit. ... For Hohmann transfer orbits, the initial orbit ...

  4. Orbital maneuver - Wikipedia

    en.wikipedia.org/wiki/Orbital_maneuver

    The orbital maneuver to perform the Hohmann transfer uses two engine impulses which move a ... Orbital inclination change is an orbital maneuver aimed at changing ...

  5. Trans-lunar injection - Wikipedia

    en.wikipedia.org/wiki/Trans-lunar_injection

    Lunar transfer, perspective view. TLI occurs at the red dot near Earth. A trans-lunar injection (TLI) is a propulsive maneuver, which is used to send a spacecraft to the Moon. Typical lunar transfer trajectories approximate Hohmann transfers, although low-energy transfers have also been used in some cases, as with the Hiten probe. [1]

  6. List of orbits - Wikipedia

    en.wikipedia.org/wiki/List_of_orbits

    Geostationary or geosynchronous transfer orbit (GTO): An elliptic orbit where the perigee is at the altitude of a low Earth orbit (LEO) and the apogee at the altitude of a geostationary orbit. Hohmann transfer orbit: An orbital maneuver that moves a spacecraft from one circular orbit to another using two engine impulses.

  7. Geostationary transfer orbit - Wikipedia

    en.wikipedia.org/wiki/Geostationary_transfer_orbit

    In case of using the Hohmann transfer orbit, only a few days are required to reach the geosynchronous orbit. By using low-thrust engines or electrical propulsion, months are required until the satellite reaches its final orbit. The orbital inclination of a GTO is the angle between the orbit plane and the Earth's equatorial plane.

  8. Orbit phasing - Wikipedia

    en.wikipedia.org/wiki/Orbit_phasing

    Remember that this change in velocity, ∆V, is only the amount required to change the spacecraft from its original orbit to the phasing orbit.A second change in velocity equal to the magnitude but opposite in direction of the first must be done after the spacecraft travels one phase orbit period to return the spacecraft from the phasing orbit to the original orbit.

  9. Orbital eccentricity - Wikipedia

    en.wikipedia.org/wiki/Orbital_eccentricity

    (Hohmann transfer orbit; ... This is a slow change in the orbit of Earth, ... provides series for Earth orbital eccentricity and orbital inclination.