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  2. Longitude of the ascending node - Wikipedia

    en.wikipedia.org/.../Longitude_of_the_ascending_node

    In this case, the longitude is also called the right ascension of the ascending node (RAAN). The angle is measured eastwards (or, as seen from the north, counterclockwise) from the FPA to the node. [2] [3] An alternative is the local time of the ascending node (LTAN), based on the local mean time at which the

  3. LTAN - Wikipedia

    en.wikipedia.org/wiki/LTAN

    Local time of the ascending node, an orbital element Topics referred to by the same term This disambiguation page lists articles associated with the title LTAN .

  4. Orbital node - Wikipedia

    en.wikipedia.org/wiki/Orbital_node

    In the case of objects outside the Solar System, the ascending node is the node where the orbiting secondary passes away from the observer, and the descending node is the node where it moves towards the observer. [5], p. 137. The position of the node may be used as one of a set of parameters, called orbital elements, which

  5. Beta angle - Wikipedia

    en.wikipedia.org/wiki/Beta_angle

    The value of a solar beta angle for a satellite in Earth orbit can be found using the equation = ⁡ [⁡ ⁡ ⁡ ⁡ ⁡ ⁡ ⁡ + ⁡ ⁡ ⁡ ()] where is the ecliptic true solar longitude, is the right ascension of ascending node (RAAN), is the orbit's inclination, and is the obliquity of the ecliptic (approximately 23.45 degrees for Earth at present).

  6. Nodal period - Wikipedia

    en.wikipedia.org/wiki/Nodal_Period

    The nodal period (or draconic period) of a satellite is the time interval between successive passages of the satellite through either of its orbital nodes, [1] [2] typically the ascending node. This type of orbital period applies to artificial satellites, like those that monitor weather on Earth , and natural satellites like the Moon .

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  8. Satellite ground track - Wikipedia

    en.wikipedia.org/wiki/Satellite_ground_track

    This ground track is shifted east or west depending on the longitude of the ascending node, which can vary over time due to perturbations of the orbit. If the period of the satellite is slightly longer than an integer fraction of a day, the ground track will shift west over time; if it is slightly shorter, the ground track will shift east. [2] [4]

  9. Sun-synchronous orbit - Wikipedia

    en.wikipedia.org/wiki/Sun-synchronous_orbit

    For example, a satellite in Sun-synchronous orbit might ascend across the equator twelve times a day, each time at approximately 15:00 mean local time. Sun-synchronous orbit from a top view of the ecliptic plane with local solar time (LST) zones for reference and a descending node of 10:30. The LST zones show how the local time beneath the ...