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12 relations: Apsis, Eccentricity vector, Geocentric orbit, Heliocentric orbit, Kepler orbit, Longitude of the ascending node, Longitude of the periapsis, Non-inclined orbit, Orbit, Orbital elements, Orbital mechanics, Orbital node.
Apsis
An apsis (ἁψίς; plural apsides, Greek: ἁψῖδες) is an extreme point in the orbit of an object.
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Eccentricity vector
In celestial mechanics, the eccentricity vector of a Kepler orbit is the dimensionless vector with direction pointing from apoapsis to periapsis and with magnitude equal to the orbit's scalar eccentricity.
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Geocentric orbit
A geocentric orbit or Earth orbit involves any object orbiting Planet Earth, such as the Moon or artificial satellites.
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Heliocentric orbit
A heliocentric orbit (also called circumsolar orbit) is an orbit around the barycenter of the Solar System, which is usually located within or very near the surface of the Sun.
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Kepler orbit
In celestial mechanics, a Kepler orbit (or Keplerian orbit) is the motion of one body relative to another, as an ellipse, parabola, or hyperbola, which forms a two-dimensional orbital plane in three-dimensional space.
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Longitude of the ascending node
The longitude of the ascending node (☊ or Ω) is one of the orbital elements used to specify the orbit of an object in space.
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Longitude of the periapsis
In celestial mechanics, the longitude of the periapsis, also called longitude of the pericenter, of an orbiting body is the longitude (measured from the point of the vernal equinox) at which the periapsis (closest approach to the central body) would occur if the body's orbit inclination were zero.
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Non-inclined orbit
A non-inclined orbit is an orbit coplanar with a plane of reference.
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Orbit
In physics, an orbit is the gravitationally curved trajectory of an object, such as the trajectory of a planet around a star or a natural satellite around a planet.
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Orbital elements
Orbital elements are the parameters required to uniquely identify a specific orbit.
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Orbital mechanics
Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft.
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Orbital node
An orbital node is either of the two points where an orbit intersects a plane of reference to which it is inclined.
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Argument of Periastron, Argument of Pericenter, Argument of Perihelion, Argument of periastron, Argument of pericenter, Argument of perifocus, Argument of perigee, Argument of perihelion, Argument of the pariapsis, Argument of the perihelion, Arguments of perihelion.
