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Domain name - apoapsis.biz

Site title - Squarespace - Website Expired

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198.185.159.144 198.49.23.144 198.49.23.145 198.185.159.145

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☆ apoapsis.biz. 3598 IN HINFO "RFC8482" ""

Domain Name: apoapsis.biz
Registry Domain ID: D9012D76CF6DA4CC6A1B5F474E0473CED-GDREG
Registrar WHOIS Server: https://porkbun.com/whois
Registrar URL: www.porkbun.com
Updated Date: 2023-10-12T04:30:33Z
Creation Date: 2023-10-07T04:30:33Z
Registry Expiry Date: 2024-10-07T04:30:33Z
Registrar: Porkbun
Registrar IANA ID: 1861
Registrar Abuse Contact Email: abuse@porkbun.com
Registrar Abuse Contact Phone: +1.5038508351
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Name Server: curitiba.ns.porkbun.com
Name Server: salvador.ns.porkbun.com
Name Server: fortaleza.ns.porkbun.com
Name Server: maceio.ns.porkbun.com
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Brief facts about apoapsis:

An apsis is the farthest or nearest point in the orbit of a planetary body about its primary body. The line of apsides is the line connecting the two extreme values. Apsides pertaining to orbits around the Sun have distinct names to differentiate themselves from other apsides; these names are aphelion for the farthest and perihelion for the nearest point in the solar orbit. The Moon's two apsides are the farthest point, apogee, and the nearest point, perigee, of its orbit around the host Earth. Earth's two apsides are the farthest point, aphelion, and the nearest point, perihelion, of its orbit around the host Sun. The terms aphelion and perihelion apply in the same way to the orbits of Jupiter and the other planets, the comets, and the asteroids of the Solar System.

Distance of closest approach - The distance of closest approach of two objects is the distance between their centers when they are externally tangent. The objects may be geometric shapes or physical particles with well-defined boundaries. The distance of closest approach is sometimes referred to as the contact distance.

Eccentric anomaly - In orbital mechanics, the eccentric anomaly is an angular parameter that defines the position of a body that is moving along an elliptic Kepler orbit.

Flyby (spaceflight) - A flyby is a spaceflight operation in which a spacecraft passes in proximity to another body, usually a target of its space exploration mission and/or a source of a gravity assist to impel it towards another target.

Mean anomaly - In celestial mechanics, the mean anomaly is the fraction of an elliptical orbit's period that has elapsed since the orbiting body passed periapsis, expressed as an angle which can be used in calculating the position of that body in the classical two-body problem.

Perifocal coordinate system - The perifocal coordinate system is a frame of reference for an orbit. The frame is centered at the focus of the orbit, i.e. the celestial body about which the orbit is centered. The unit vectors \old{\hat{p}} and \old{\hat{q}} lie in the plane of the orbit.

True anomaly - In celestial mechanics, true anomaly is an angular parameter that defines the position of a body moving along a Keplerian orbit. It is the angle between the direction of periapsis and the current position of the body, as seen from the main focus of the ellipse.

Orbits