apoapsis


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Related to apoapsis: periapsis

ap·o·ap·sis

 (ăp′ō-ăp′sĭs)
n. pl. ap·o·ap·si·des (-ăp′sĭ-dēz′)
The point at which an orbiting object is farthest away from the center of mass of the body it is orbiting.
American Heritage® Dictionary of the English Language, Fifth Edition. Copyright © 2016 by Houghton Mifflin Harcourt Publishing Company. Published by Houghton Mifflin Harcourt Publishing Company. All rights reserved.

apoapsis

(ˌæpəʊˈæpsɪs)
n
the point in an elliptical orbit which is farthest from the object being orbited
Collins English Dictionary – Complete and Unabridged, 12th Edition 2014 © HarperCollins Publishers 1991, 1994, 1998, 2000, 2003, 2006, 2007, 2009, 2011, 2014
ThesaurusAntonymsRelated WordsSynonymsLegend:
Noun1.apoapsis - (astronomy) the point in an orbit farthest from the body being orbitedapoapsis - (astronomy) the point in an orbit farthest from the body being orbited
astronomy, uranology - the branch of physics that studies celestial bodies and the universe as a whole
apogee - apoapsis in Earth orbit; the point in its orbit where a satellite is at the greatest distance from the Earth
aphelion - apoapsis in solar orbit; the point in the orbit of a planet or comet that is at the greatest distance from the sun
apojove - apoapsis in orbit around Jupiter
apolune, aposelene - apoapsis in orbit around the moon
celestial point - a point in the heavens (on the celestial sphere)
celestial orbit, orbit - the (usually elliptical) path described by one celestial body in its revolution about another; "he plotted the orbit of the moon"
periapsis, point of periapsis - (astronomy) the point in an orbit closest to the body being orbited
Based on WordNet 3.0, Farlex clipart collection. © 2003-2012 Princeton University, Farlex Inc.
Translations
References in periodicals archive ?
The apoapsis altitude (highest point in orbit) dropped from about 6050 to about 4570 km, an orbit change that improves MAVEN's availability to support relay communications with NASA's landers and rovers on the surface of Mars.
A deep-space maneuver is performed near the apoapsis in order to modify [v.sub.[infinity]] (increase, if one is considering an escape trajectory, or decrease, if one instead considers a capture) at the next encounter of the probe with the secondary body.
With this aim, we know that a bad distribution of the points in the periapsis and the apoapsis leads inexorably to truncation errors of such magnitude that make impossible the task proposed regarding the reduction of errors.