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  2. List of orbits - Wikipedia

    en.wikipedia.org/wiki/List_of_orbits

    Orbits around the L 1 point are used by spacecraft that want a constant view of the Sun, such as the Solar and Heliospheric Observatory. Orbits around L 2 are used by missions that always want both Earth and the Sun behind them. This enables a single shield to block radiation from both Earth and the Sun, allowing passive cooling of sensitive ...

  3. List of Solar System probes - Wikipedia

    en.wikipedia.org/wiki/List_of_Solar_System_probes

    This is a list of space probes that have left Earth orbit (or were launched with that intention but failed), organized by their planned destination. It includes planetary probes, solar probes, and probes to asteroids and comets, but excludes lunar missions, which are listed separately at List of lunar probes and List of Apollo missions.

  4. Category:Orbits - Wikipedia

    en.wikipedia.org/wiki/Category:Orbits

    Download as PDF; Printable version; In other projects Wikimedia Commons; Wikidata item; ... Pages in category "Orbits" The following 121 pages are in this category ...

  5. List of extraterrestrial orbiters - Wikipedia

    en.wikipedia.org/wiki/List_of_extraterrestrial...

    First lunar sample return mission from far side and south pole of Moon by China. Ascent stage was be deorbited on 6 June 2024. Capsule was be returned sample via service module on 25 June 2024. [12] ICUBE-Q: Pakistan 8 May 2024 On a Selenocentric orbit: First Pakistani lunar mission, piggybacking with Chang'e 6. [13] Blue Ghost M1: USA

  6. Two-line element set - Wikipedia

    en.wikipedia.org/wiki/Two-line_element_set

    A two-line element set (TLE, or more rarely 2LE) or three-line element set (3LE) is a data format encoding a list of orbital elements of an Earth-orbiting object for a given point in time, the epoch. Using a suitable prediction formula, the state (position and velocity) at any point in the past or future can be estimated to some accuracy.

  7. Orbital state vectors - Wikipedia

    en.wikipedia.org/wiki/Orbital_state_vectors

    Orbital position vector, orbital velocity vector, other orbital elements. In astrodynamics and celestial dynamics, the orbital state vectors (sometimes state vectors) of an orbit are Cartesian vectors of position and velocity that together with their time () uniquely determine the trajectory of the orbiting body in space.

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    mail.aol.com

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  9. Longitude of the ascending node - Wikipedia

    en.wikipedia.org/wiki/Longitude_of_the_ascending...

    For orbits outside the Solar System, the plane tangent to the celestial sphere at the point of interest (called the plane of the sky) as the reference plane, and north (i.e. the perpendicular projection of the direction from the observer to the north celestial pole onto the plane of the sky) as the origin of longitude. The angle is measured ...