Orbital elements (redirect from Elements of an orbit) angles of inclination, longitude of the ascending node, and argument of periapsis can also be described as the Euler angles defining the orientation of the... 23 KB (2,924 words) - 15:29, 22 April 2024 |
Vanth (moon) (redirect from Moons of Orcus) 328°±51°.: 67 The longitude of periapsis is the sum of the ascending node and argument of periapsis, so subtracting Vanth's ascending node of 53.49°±0.33°... 35 KB (3,367 words) - 16:47, 15 April 2024 |
Dysnomia (moon) (redirect from Moons of Eris) of periapsis, so subtracting Dysnomia's ascending node of 126.17°±0.26° from its longitude of periapsis gives 180.83° for its argument of periapsis. Dysnomia's... 21 KB (1,965 words) - 09:46, 4 March 2024 |
so-called longitude of the periapsis (also called longitude of the pericenter). For the orbit of the Earth, this is called the longitude of perihelion... 42 KB (3,866 words) - 20:56, 25 April 2024 |
true anomaly, ϖ ≡ ω + Ω is the longitude of orbit's periapsis, ω is the argument of periapsis, and Ω is the longitude of the orbit's ascending node, Multon... 2 KB (156 words) - 01:31, 30 November 2023 |
Mean longitude is the ecliptic longitude at which an orbiting body could be found if its orbit were circular and free of perturbations. While nominally... 5 KB (576 words) - 09:55, 26 March 2024 |