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Semi-major and semi-minor axes
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thus runs from the centre, through a focus, and to the perimeter. The semi-minor axis (minor semiaxis) of an ellipse or hyperbola is a line segment thatEccentric anomaly (1,010 words) [view diff] exact match in snippet view article find links to article
{y^{2}}{b^{2}}}=1,} where a is the semi-major axis and b is the semi-minor axis. For a point on the ellipse, P = P(x, y), representing the positionSpheroid (1,926 words) [view diff] exact match in snippet view article find links to article
rotation about the z-axis of an ellipse with semi-major axis a and semi-minor axis c, therefore e may be identified as the eccentricity. (See ellipseSpecific angular momentum (1,221 words) [view diff] exact match in snippet view article find links to article
for the area πab{\displaystyle \pi ab} of an ellipse. Replacing the semi-minor axis with b=ap{\displaystyle b={\sqrt {ap}}} and the specific relative angularSemi-synchronous orbit (113 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOsculating orbit (824 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital period (2,020 words) [view diff] exact match in snippet view article find links to article
The semi-major axis (a) and semi-minor axis (b) of an ellipseSubsynchronous orbit (153 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentTrue longitude (156 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentRadial trajectory (1,299 words) [view diff] exact match in snippet view article find links to article
objects is less than the escape velocity. This is an elliptic orbit with semi-minor axis = 0 and eccentricity = 1. Although the eccentricity is 1, this is notAreocentric orbit (204 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentList of orbits (3,471 words) [view diff] exact match in snippet view article find links to article
moving at less than the escape velocity. This is an elliptic orbit with semi-minor axis = 0 and eccentricity = 1. Although the eccentricity is 1, this is notPolar orbit (416 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentInclined orbit (336 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLongitude of the ascending node (655 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentGeodetic datum (3,073 words) [view diff] exact match in snippet view article find links to article
a{\displaystyle a} and f{\displaystyle f} it is possible to derive the semi-minor axis b{\displaystyle b}, first eccentricity e{\displaystyle e} and secondHighly elliptical orbit (242 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentElliptic orbit (2,592 words) [view diff] exact match in snippet view article find links to article
trajectory can be a double line segment, which is a degenerate ellipse with semi-minor axis = 0 and eccentricity = 1. Although the eccentricity is 1, this is notMean longitude (576 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentArgument of periapsis (557 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentBox orbit (179 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHeliocentric orbit (381 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentMean anomaly (1,244 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentSynchronous orbit (562 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentGraveyard orbit (998 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital inclination (1,465 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentMedium Earth orbit (989 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentParking orbit (855 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentCharacteristic energy (661 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital state vectors (826 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentAreostationary orbit (577 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentSquare kilometre (1,513 words) [view diff] exact match in snippet view article find links to article
2.53 kilometres (1.57 mi). The maximum distance from east to west (semi-minor axis) is 1.81 kilometres (1.12 mi). A perfect ellipse of these dimensionsAreosynchronous orbit (377 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLongitude of the periapsis (606 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLow-energy transfer (825 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentTrue anomaly (1,020 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentEllipse (14,138 words) [view diff] exact match in snippet view article find links to article
coefficients can be obtained from known semi-major axis a{\displaystyle a}, semi-minor axis b{\displaystyle b}, center coordinates (x∘,y∘){\displaystyle \left(x_{\circLatitude (6,180 words) [view diff] exact match in snippet view article find links to article
semi-major axis, a. The other parameter is usually (1) the polar radius or semi-minor axis, b; or (2) the (first) flattening, f; or (3) the eccentricity, e. TheseCircular orbit (1,178 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHalo orbit (1,104 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLissajous orbit (766 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLow Earth orbit (2,090 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHigh Earth orbit (565 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentSun-synchronous orbit (1,582 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentParabolic trajectory (1,010 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital inclination change (940 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLunar orbit (1,730 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLine segment (1,484 words) [view diff] exact match in snippet view article find links to article
midpoint (the ellipse's center) to either of its endpoints is called a semi-minor axis. The chords of an ellipse which are perpendicular to the major axisGeostationary transfer orbit (1,727 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentBINGO (telescope) (2,635 words) [view diff] exact match in snippet view article
radiation from the sky. The primary mirror has a paraboloidal shape with a semi-minor axis of 20 meters radius, and its function is to capture the radiation.Orbital speed (1,358 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentRosetta orbit (321 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentNear-equatorial orbit (689 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentCylinder (2,805 words) [view diff] exact match in snippet view article find links to article
example, an elliptic cylinder with a base having semi-major axis a, semi-minor axis b and height h has a volume V = Ah, where A is the area of the baseGeocentric orbit (1,997 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentVis-viva equation (1,235 words) [view diff] exact match in snippet view article find links to article
rarp=b2{\displaystyle r_{a}r_{p}=b^{2}}, where a is semi-major axis and b is semi-minor axis of the elliptical orbit, as follows: va2=GM(2ra−1a)=GMa(2a−rara)=GEarth's orbit (1,829 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentMaclaurin spheroid (604 words) [view diff] exact match in snippet view article find links to article
spheroid with equatorial semi-major axis a{\displaystyle a} and polar semi-minor axis c{\displaystyle c}, the angular velocity Ω{\displaystyle \Omega } aboutOrbital spaceflight (1,404 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbit equation (1,269 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentEphemeris (1,697 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentTrans-lunar injection (1,336 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentStandard gravitational parameter (1,433 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentDistant retrograde orbit (960 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentEuropean Terrestrial Reference System 1989 (585 words) [view diff] case mismatch in snippet view article find links to article
4258) Spheroid GRS 1980 (EPSG ID 7019) Semi-Major Axis 6378137.000 Semi-Minor Axis 6356752.314140 Inverse flattening 298.257222101 Prime Meridian GreenwichTundra orbit (1,697 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital eccentricity (2,645 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLaunch window (1,271 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentPerturbation (astronomy) (2,338 words) [view diff] exact match in snippet view article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital elements (2,805 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentInterplanetary Transport Network (1,842 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentDelta-v (2,105 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHorseshoe orbit (1,341 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentFigure of the Earth (2,810 words) [view diff] exact match in snippet view article find links to article
and b{\displaystyle b} is the distance from the center to the pole. (semi-minor axis) It was stated earlier that measurements are made on the apparent orNear-rectilinear halo orbit (931 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentGround track (1,964 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOberth effect (1,912 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital maneuver (2,121 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentSpecific orbital energy (1,841 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentTwo-line element set (1,737 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentConic section (8,942 words) [view diff] exact match in snippet view article find links to article
is the shortest diameter of an ellipse, and its half-length is the semi-minor axis (b), the same value b as in the standard equation below. By analogyAstronomical coordinate systems (3,840 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentConic section (8,942 words) [view diff] exact match in snippet view article find links to article
is the shortest diameter of an ellipse, and its half-length is the semi-minor axis (b), the same value b as in the standard equation below. By analogyGeosynchronous orbit (3,171 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentEpoch (astronomy) (3,437 words) [view diff] exact match in snippet view article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentMolniya orbit (3,090 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentEscape velocity (3,520 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbital station-keeping (1,752 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLibration point orbit (306 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentTransatmospheric orbit (358 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentBi-elliptic transfer (1,947 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbit of the Moon (4,652 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentVincenty's formulae (2,359 words) [view diff] exact match in snippet view article find links to article
the ellipsoid; (1/298.257223563 in WGS-84) b = (1 − ƒ) a length of semi-minor axis of the ellipsoid (radius at the poles); (6356752.314245 meters in WGS-84)Geostationary orbit (4,806 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentGeodesy (4,184 words) [view diff] exact match in snippet view article find links to article
radius) a and flattening f. The quantity f = a − b/a, where b is the semi-minor axis (polar radius), is purely geometrical. The mechanical ellipticity ofHyperboloid (2,476 words) [view diff] exact match in snippet view article find links to article
one-sheet hyperboloid of revolution is rotating a hyperbola around its semi-minor axis (see picture; rotating the hyperbola around its other axis gives aTsiolkovsky rocket equation (3,978 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHubble sequence (3,078 words) [view diff] exact match in snippet view article find links to article
b / a for an ellipse with a the semi-major axis length and b the semi-minor axis length. The ellipticity increases from left to right on the HubbleOrbital mechanics (5,628 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentSpace rendezvous (3,698 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentLagrange point (5,705 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHill sphere (2,856 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentOrbit phasing (1,095 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHohmann transfer orbit (3,588 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentGravity assist (5,021 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentHyperbola (12,178 words) [view diff] exact match in snippet view article find links to article
coefficients can be obtained from known semi-major axis a,{\displaystyle a,} semi-minor axis b,{\displaystyle b,} center coordinates (x∘,y∘){\displaystyle (x_{\circOrbit (7,955 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentScientific law (5,597 words) [view diff] exact match in snippet view article find links to article
is the eccentricity of the elliptic orbit, of semi-major axis a and semi-minor axis b, and ℓ is the semi-latus rectum. This equation in itself is nothingDelta-v budget (2,719 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentGravity turn (3,406 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentN-body problem (8,459 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentCurve of constant width (3,573 words) [view diff] exact match in snippet view article find links to article
{3}}}. Equivalently, the semi-major axis should be at most twice the semi-minor axis. Given any two bodies of constant width, their Minkowski sum formsJapanese tree frog (3,382 words) [view diff] exact match in snippet view article find links to article
distance between posterior corners of eyes (EPD), distance between semi-minor axis of the upper eye (LILe), angle between the two lines that connect thePi (17,361 words) [view diff] exact match in snippet view article find links to article
radius r is πr2. The area of an ellipse with semi-major axis a and semi-minor axis b is πab. The volume of a sphere with radius r is 4/3πr3. The surfaceTheoretical gravity (3,502 words) [view diff] exact match in snippet view article find links to article
= Normal gravity at poles a = semi-major axis (Equator radius) b = semi-minor axis (pole radius) φ {\displaystyle \varphi } = latitude Due to numericalDegenerate conic (2,544 words) [view diff] exact match in snippet view article find links to article
the foci is mandated to equal the interfocal distance; thus it has semi-minor axis equal to zero and has eccentricity equal to one. The result is a lineKepler orbit (5,689 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentElliptic integral (6,618 words) [view diff] exact match in snippet view article find links to article
}{2}},k\right)=E(1;k).} For an ellipse with semi-major axis a and semi-minor axis b and eccentricity e = √1 − b2/a2, the complete elliptic integral ofConfocal conic sections (3,382 words) [view diff] exact match in snippet view article find links to article
confocal with a given ellipse of semi-major axis a{\displaystyle a} and semi-minor axis b{\displaystyle b} (so that 0<b<a{\displaystyle 0<b<a}), each conicLambert's problem (2,170 words) [view diff] exact match in snippet view article find links to article
above is The eccentricity (with sign!) for the hyperbola is and the semi-minor axis is The coordinates of the point F1{\displaystyle F_{1}} relative theUngula (2,558 words) [view diff] exact match in snippet view article find links to article
r^{2}}, and the slanted top of the said ungula is a half-ellipse with semi-minor axis of length r and semi-major axis of length r1+k2{\displaystyle r{\sqrtList of formulae involving π (6,872 words) [view diff] exact match in snippet view article find links to article
where A is the area enclosed by an ellipse with semi-major axis a and semi-minor axis b. A = 4 π r 2 {\displaystyle A=4\pi r^{2}} where A is the area betweenDupin cyclide (4,594 words) [view diff] no match in snippet view article find links to article
a {\displaystyle a} is the semi major and b {\displaystyle b} the semi minor axis. c {\displaystyle c} is the linear eccentricity of the ellipse. Hence:Very low Earth orbit (1,854 words) [view diff] exact match in snippet view article find links to article
Shape Size e Eccentricity a Semi-major axis b Semi-minor axis Q, q Apsides Orientation i Inclination Ω Longitude of the ascending node ω ArgumentEarth section paths (5,831 words) [view diff] exact match in snippet view article find links to article
{i}}^{*}} =\left({\frac {m}{p}},{\frac {-l}{p}},0\right)}, and the semi-minor axis is b∗=bCa∗{\textstyle b^{*}={\frac {b}{\sqrt {C}}}a^{*}}, in the direction