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  2. Bi-elliptic transfer - Wikipedia

    en.wikipedia.org/wiki/Bi-elliptic_transfer

    A bi-elliptic transfer from a low circular starting orbit (blue) to a higher circular orbit (red) Comparable Hohmann transfer orbit (2), from a low circular orbit (1) to a higher orbit (3) In astronautics and aerospace engineering , the bi-elliptic transfer is an orbital maneuver that moves a spacecraft from one orbit to another and may, in ...

  3. 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).

  4. Transfer orbit - Wikipedia

    en.wikipedia.org/wiki/Transfer_orbit

    In orbital mechanics, a transfer orbit is an intermediate elliptical orbit that is used to move a spacecraft in an orbital maneuver from one circular, or largely circular, orbit to another. There are several types of transfer orbits, which vary in their energy efficiency and speed of transfer.

  5. 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.

  6. Spacecraft flight dynamics - Wikipedia

    en.wikipedia.org/wiki/Spacecraft_flight_dynamics

    Hohmann transfer orbit, 2, from an orbit (1) to a higher orbit (3) A Hohmann transfer orbit is the simplest maneuver which can be used to move a spacecraft from one altitude to another. Two burns are required: the first to send the craft into the elliptical transfer orbit, and a second to circularize the target orbit.

  7. Iran launches advanced module to deploy satellites to higher ...

    www.aol.com/news/iran-launches-advanced-module...

    The Samān-1 transfer module, along with a CubeSat and a research payload "were successfully placed in an elliptical orbit with a high point of 410 km (255 miles) and a low point of 300 km," said ...

  8. Orbital mechanics - Wikipedia

    en.wikipedia.org/wiki/Orbital_mechanics

    The Hohmann transfer orbit requires a minimal delta-v. A bi-elliptic transfer can require less energy than the Hohmann transfer, if the ratio of orbits is 11.94 or greater, [5] but comes at the cost of increased trip time over the Hohmann transfer.

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