Orbital eccentricity - wikipedia Orbital eccentricity This article is about eccentricity in astrodynamics. For other uses, see Eccentricity ( disambiguation ). An elliptic, parabolic and hyperbolic Kepler orbit : elliptic ( eccentricity = 0.7 ) parabolic ( eccentricity = 1 ) hyperbolic orbit ( eccentricity = 1.3 ) The orbital eccentricity of an astronomical object is a parameter that determines the amount by which its orbit around another body deviates from a perfect circle. A value of 0 is a circular orbit, values between 0 and 1 form an elliptical orbit, 1 is a parabolic escape orbit, and greater than 1 is a hyperbola. The term derives its name from the parameters of conic sections, as every Kepler orbit is a conic section. It is normally used for the isolated two - body problem, but extensions exist for objects following a rosette orbit through the galaxy. Contents 1 Definition 2 Etymology 3 Calculation 4 Examples 5 Mean eccentricity 6 Climatic effect 7 Exoplanets 8 See also 9 References 10 External links Definition e = 0 e = 0.5 Orbits in a two - body system for two values of the eccentricity, e. In a two - body problem with inverse - square - law force, every orbit is a Kepler orbit. The eccentricity of this Kepler orbit is a non-negative number that defines its shape. The eccentricity may take the following values : circular orbit : e = 0 elliptic orbit : 0 < e < 1 ( see ellipse ) parabolic trajectory : e = 1 ( see parabola ) hyperbolic trajectory : e > 1 ( see hyperbola ) The eccentricity e is given by e = 1 + 2 E L 2 m red α 2 ( displaystyle e = ( sqrt ( 1 + ( \frac ( 2EL ^ ( 2 ) ) ( m_ ( \text ( red ) ) alpha ^ ( 2 ) ) ) ) ) ) where E is the total orbital energy, L is the angular momentum, m is the reduced mass, and α the coefficient of the inverse - square law central force such as gravity or electrostatics in classical physics : F = α r 2 ( displaystyle F = ( \frac ( alpha ) ( r ^ ( 2 ) ) ) ) ( α is negative for an attractive force, positive for a repulsive one ; see also Kepler problem ) or in the case of a gravitational force : e = 1 + 2 ε h 2 μ 2 ( displaystyle e = ( sqrt ( 1 + ( \frac ( 2 \varepsilon h ^ ( 2 ) ) ( mu ^ ( 2 ) ) ) ) ) ) where ε is the specific orbital energy ( total energy divided by the reduced mass ), μ the standard gravitational parameter based on the total mass, and h the specific relative angular momentum ( angular momentum divided by the reduced mass ). For values of e from 0 to 1 the orbit 's shape is an increasingly elongated ( or flatter ) ellipse ; for values of e from 1 to infinity the orbit is a hyperbola branch making a total turn of 2 arccsc e, decreasing from 180 to 0 degrees. The limit case between an ellipse and a hyperbola, when e equals 1, is parabola. Radial trajectories are classified as elliptic, parabolic, or hyperbolic based on the energy of the orbit, not the eccentricity. Radial orbits have zero angular momentum and hence eccentricity equal to one. Keeping the energy constant and reducing the angular momentum, elliptic, parabolic, and hyperbolic orbits each tend to the corresponding type of radial trajectory while e tends to 1 ( or in the parabolic case, remains 1 ). For a repulsive force only the hyperbolic trajectory, including the radial version, is applicable. For elliptical orbits, a simple proof shows that arcsin ( e ( displaystyle e ) ) yields the projection angle of a perfect circle to an ellipse of eccentricity e. For example, to view the eccentricity of the planet Mercury ( e = 0.2056 ), one must simply calculate the inverse sine to find the projection angle of 11.86 degrees. Next, tilt any circular object ( such as a coffee mug viewed from the top ) by that angle and the apparent ellipse projected to your eye will be of that same eccentricity. Etymology From Medieval Latin eccentricus, derived from Greek ἔκκεντρος ekkentros `` out of the center '', from ἐκ - ek -, `` out of '' + κέντρον kentron `` center ''. Eccentric first appeared in English in 1551, with the definition `` a circle in which the earth, sun. etc. deviates from its center. '' Five years later, in 1556, an adjective form of the word was added. Calculation The eccentricity of an orbit can be calculated from the orbital state vectors as the magnitude of the eccentricity vector : e = e ( displaystyle e = left mathbf ( e ) \right ) where : e is the eccentricity vector. For elliptical orbits it can also be calculated from the periapsis and apoapsis since r = a ( 1 − e ) and r = a ( 1 + e ), where a is the semimajor axis. e = r a − r p r a + r p = 1 − 2 r a r p + 1 ( displaystyle ( \begin ( aligned ) e& = ( ( r_ ( \text ( a ) ) - r_ ( \text ( p ) ) ) over ( r_ ( \text ( a ) ) + r_ ( \text ( p ) ) ) ) & = 1 - ( \frac ( 2 ) ( ( \frac ( r_ ( \text ( a ) ) ) ( r_ ( \text ( p ) ) ) ) + 1 ) ) end ( aligned ) ) ) where : r is the radius at apoapsis ( i.e., the farthest distance of the orbit to the center of mass of the system, which is a focus of the ellipse ). r is the radius at periapsis ( the closest distance ). The eccentricity of an elliptical orbit can also be used to obtain the ratio of the periapsis to the apoapsis : r p r a = 1 − e 1 + e ( displaystyle ( ( r_ ( \text ( p ) ) ) over ( r_ ( \text ( a ) ) ) ) = ( ( 1 - e ) over ( 1 + e ) ) ) For Earth, orbital eccentricity ≈ 0.0167, apoapsis = aphelion = apogee and periapsis = perihelion = perigee relative to sun. For Earth 's annual orbit path, r / r ratio = longest_radius / shortest_radius ≈ 1.034 relative to center point of path. Examples Gravity Simulator plot of the changing orbital eccentricity of Mercury, Venus, Earth, and Mars over the next 50,000 years. The arrows indicate the different scales used. The 0 point on this plot is the year 2007. Eccentricities of Solar System bodies Object eccentricity Triton 0.00002 Venus 0.0068 Neptune 0.0086 Earth 0.0167 Titan 0.0288 Uranus 0.0472 Jupiter 0.0484 Saturn 0.0541 Moon 0.0549 1 Ceres 0.0758 4 Vesta 0.0887 Mars 0.0934 10 Hygiea 0.1146 Makemake 0.1559 Haumea 0.1887 Mercury 0.2056 2 Pallas 0.2313 Pluto 0.2488 3 Juno 0.2555 324 Bamberga 0.3400 Eris 0.4407 Nereid 0.7507 Sedna 0.8549 Halley 's Comet 0.9671 Comet Hale - Bopp 0.9951 Comet Ikeya - Seki 0.9999 The eccentricity of the Earth 's orbit is currently about 0.0167 ; the Earth 's orbit is nearly circular. Venus and Neptune have even lower eccentricities. Over hundreds of thousands of years, the eccentricity of the Earth 's orbit varies from nearly 0.0034 to almost 0.058 as a result of gravitational attractions among the planets ( see graph ). The table lists the values for all planets and dwarf planets, and selected asteroid, comets and moons. Mercury has the greatest orbital eccentricity of any planet in the Solar System ( e = 0.2056 ). Such eccentricity is sufficient for Mercury to receive twice as much solar irradiation at perihelion compared to aphelion. Before its demotion from planet status in 2006, Pluto was considered to be the planet with the most eccentric orbit ( e = 0.248 ). Other Trans - Neptunian objects have significant eccentricity, notably the dwarf planet Eris ( 0.44 ). Even further out, Sedna, has an extremely high eccentricity of 6999855000000000000 ♠ 0.855 due to its estimated aphelion of 937 AU and perihelion of about 76 AU. Most of the Solar System 's asteroids have orbital eccentricities between 0 and 0.35 with an average value of 0.17. Their comparatively high eccentricities are probably due to the influence of Jupiter and to past collisions. The Moon 's value is 0.0549, the most eccentric of the large moons of the Solar System. The four Galilean moons have eccentricity < 0.01. Neptune 's largest moon Triton has an eccentricity of 6995160000000000000 ♠ 1.6 × 10 ( 6995160000000000000 ♠ 0.000 016 ), the smallest eccentricity of any known body in the Solar System ; its orbit is as close to a perfect circle as can be currently measured. However, smaller moons, particularly irregular moons, can have significant eccentricity, such as Neptune 's third largest moon Nereid ( 0.75 ). Comets have very different values of eccentricity. Periodic comets have eccentricities mostly between 0.2 and 0.7, but some of them have highly eccentric elliptical orbits with eccentricities just below 1, for example, Halley 's Comet has a value of 0.967. Non-periodic comets follow near - parabolic orbits and thus have eccentricities even closer to 1. Examples include Comet Hale -- Bopp with a value of 0.995 and comet C / 2006 P1 ( McNaught ) with a value of 7000100001900000000 ♠ 1.000 019. As Hale -- Bopp 's value is less than 1, its orbit is elliptical and it will in fact return. Comet McNaught has a hyperbolic orbit while within the influence of the planets, but is still bound to the Sun with an orbital period of about 10 years. As of a 2010 Epoch, Comet C / 1980 E1 has the largest eccentricity of any known hyperbolic comet with an eccentricity of 1.057, and will leave the Solar System indefinitely. Mean eccentricity The mean eccentricity of an object is the average eccentricity as a result of perturbations over a given time period. Neptune currently has an instant ( current Epoch ) eccentricity of 0.0113, but from 1800 to 2050 has a mean eccentricity of 6997859000000000000 ♠ 0.008 59. Climatic effect Orbital mechanics require that the duration of the seasons be proportional to the area of the Earth 's orbit swept between the solstices and equinoxes, so when the orbital eccentricity is extreme, the seasons that occur on the far side of the orbit ( aphelion ) can be substantially longer in duration. Today, northern hemisphere fall and winter occur at closest approach ( perihelion ), when the earth is moving at its maximum velocity -- while the opposite occurs in the southern hemisphere. As a result, in the northern hemisphere, fall and winter are slightly shorter than spring and summer -- but in global terms this is balanced with them being longer below the equator. In 2006, the northern hemisphere summer was 4.66 days longer than winter, and spring was 2.9 days longer than fall due to the Milankovitch cycles. Apsidal precession also slowly changes the place in the Earth 's orbit where the solstices and equinoxes occur. Note that this is a slow change in the orbit of the Earth, not the axis of rotation, which is referred to as axial precession ( see Precession § Astronomy ). Over the next 10,000 years, the northern hemisphere winters will become gradually longer and summers will become shorter. However, any cooling effect in one hemisphere is balanced by warming in the other, and any overall change will be counteracted by the fact that the eccentricity of Earth 's orbit will be almost halved. This will reduce the mean orbital radius and raise temperatures in both hemispheres closer to the mid-interglacial peak. Exoplanets Of the many exoplanets discovered, most exoplanets have a higher orbital eccentricity than our solar system. Exoplanets found with low orbital eccentricity, near circular orbits, are very close to its star and are tidally locked to the star. All eight planets in the Solar System have near - circular orbits. The exoplanets discovered show that the solar system, with its unusually low eccentricity, is rare and unique. One theory attributes this low eccentricity to the high number of planets in the Solar System ; another suggests it arose because of its unique asteroid belts. A few other multiplanetary systems have been found, but none resemble the Solar System. The Solar System has unique planetesimal systems, which led the planets to have near - circular orbits. Solar planetesimal systems include the asteroid belt, Hilda family, Kuiper belt, Hills cloud, and the Oort cloud. The exoplanet systems discovered have either no planetesimal systems or one very large planetesimal system. Low eccentricity is needed for habitability, especially advanced life. High multiplicity planet systems are much more likely to have habitable exoplanets. The grand tack hypothesis of the Solar System also helps understand its near - circular orbits and other unique features. See also Eccentricity ( mathematics ) Eccentricity vector Equation of time Milankovitch cycles Orbits References Jump up ^ A. Berger & M.F. Loutre ( 1991 ). `` Graph of the eccentricity of the Earth 's orbit ''. Illinois State Museum ( Insolation values for the climate of the last 10 million years ). Retrieved 2009 - 12 - 17. Jump up ^ Asteroids Jump up ^ David R. Williams ( 22 January 2008 ). `` Neptunian Satellite Fact Sheet ''. NASA. Retrieved 2009 - 12 - 17. Jump up ^ Lewis, John ( 2 December 2012 ). Physics and Chemistry of the Solar System. Academic Press. Retrieved 2015 - 03 - 29. ^ Jump up to : `` JPL Small - Body Database Browser : C / 1995 O1 ( Hale - Bopp ) '' ( 2007 - 10 - 22 last obs ). Retrieved 2008 - 12 - 05. Jump up ^ `` JPL Small - Body Database Browser : C / 2006 P1 ( McNaught ) '' ( 2007 - 07 - 11 last obs ). Retrieved 2009 - 12 - 17. Jump up ^ `` Comet C / 2006 P1 ( McNaught ) - facts and figures ''. Perth Observatory in Australia. 2007 - 01 - 22. Retrieved 2011 - 02 - 01. Jump up ^ `` JPL Small - Body Database Browser : C / 1980 E1 ( Bowell ) '' ( 1986 - 12 - 02 last obs ). Retrieved 2010 - 03 - 22. Jump up ^ Williams, David R. ( 2007 - 11 - 29 ). `` Neptune Fact Sheet ''. NASA. Retrieved 2009 - 12 - 17. Jump up ^ `` Keplerian elements for 1800 A.D. to 2050 A.D. ''. JPL Solar System Dynamics. Retrieved 2009 - 12 - 17. Jump up ^ Data from United States Naval Observatory Jump up ^ Berger A. ; Loutre M.F. ; Mélice J.L. ( 2006 ). `` Equatorial insolation : from precession harmonics to eccentricity frequencies '' ( PDF ). Clim. Past Discuss. 2 ( 4 ) : 519 -- 533. doi : 10.5194 / cpd - 2 - 519 - 2006. Jump up ^ Arizona U., Long Term Climate Jump up ^ exoplanets.org, ORBITAL ECCENTRICITES, by G. Marcy, P. Butler, D. Fischer, S. Vogt, 20 Sept 2003 Jump up ^ Ward, Peter ; Brownlee, Donald ( 2000 ). Rare Earth : Why Complex Life is Uncommon in the Universe. Springer. pp. 122 -- 123. ISBN 0 - 387 - 98701 - 0. Jump up ^ Limbach, MA ; Turner, EL. `` Exoplanet orbital eccentricity : multiplicity relation and the Solar System ''. Proc Natl Acad Sci USA. 112 : 20 -- 4. Bibcode : 2015PNAS... 112... 20L. PMC 4291657. PMID 25512527. arXiv : 1404.2552. doi : 10.1073 / pnas. 1406545111. Jump up ^ Steward Observatory, University of Arizona, Tucson, Planetesimals in Debris Disks, by Andrew N. Youdin and George H. Rieke, 2015 Jump up ^ Zubritsky, Elizabeth. `` Jupiter 's Youthful Travels Redefined Solar System ''. NASA. Retrieved 4 November 2015. Jump up ^ Sanders, Ray. `` How Did Jupiter Shape Our Solar System ? ''. Universe Today. Retrieved 4 November 2015. Jump up ^ Choi, Charles Q. `` Jupiter 's ' Smashing ' Migration May Explain Our Oddball Solar System ''. Space.com. Retrieved 4 November 2015. Jump up ^ Davidsson, Dr. Björn J.R. `` Mysteries of the asteroid belt ''. The History of the Solar System. Retrieved 7 November 2015. Jump up ^ Raymond, Sean. `` The Grand Tack ''. PlanetPlanet. Retrieved 7 November 2015. Jump up ^ O'Brien, David P. ; Walsh, Kevin J. ; Morbidelli, Alessandro ; Raymond, Sean N. ; Mandell, Avi M. ( 2014 ). `` Water delivery and giant impacts in the ' Grand Tack ' scenario ''. Icarus. 239 : 74 -- 84. Bibcode : 2014Icar... 239... 74O. arXiv : 1407.3290. doi : 10.1016 / j. icarus. 2014.05. 009. Jump up ^ Relative Likelihood for Life as a Function of Cosmic Time, Journal of Cosmology and Astroparticle Physics, by Abraham Loeb, Rafael Batista, and David Sloan, August 2016, doi : 10.1088 / 1475 - 7516 / 2016 / 08 / 040 Jump up ^ Harvard - Smithsonian Center for Astrophysics, `` Is Earthly Life Premature from a Cosmic Perspective ? '', August 1, 2016 Jump up ^ Relative Likelihood, by Loeb, Batista, and Sloan Prussing, John E., and Bruce A. Conway. Orbital Mechanics. New York : Oxford University Press, 1993. External links World of Physics : Eccentricity The NOAA page on Climate Forcing Data includes ( calculated ) data from Berger ( 1978 ), Berger and Loutre ( 1991 ). Laskar et al. ( 2004 ) on Earth orbital variations, Includes eccentricity over the last 50 million years and for the coming 20 million years. The orbital simulations by Varadi, Ghil and Runnegar ( 2003 ) provides series for Earth orbital eccentricity and orbital inclination. Kepler 's Second law 's simulation Gravitational orbits Types General Box Capture Circular Elliptical / Highly elliptical Escape Graveyard Hyperbolic trajectory Inclined / Non-inclined Osculating Parabolic trajectory Parking Synchronous semi sub Transfer orbit Geocentric Geosynchronous Geostationary Sun - synchronous Low Earth Medium Earth High Earth Molniya Near - equatorial Orbit of the Moon Polar Tundra About other points Areosynchronous Areostationary Halo Lissajous Lunar Heliocentric Heliosynchronous Parameters 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 Argument of periapsis π Longitude of the periapsis Position M Mean anomaly ν True anomaly E Eccentric anomaly L Mean longitude l True longitude Variation T Orbital period n Mean motion v Orbital speed t Epoch Maneuvers Collision avoidance ( spacecraft ) Delta - v Delta - v budget Bi-elliptic transfer Geostationary transfer Gravity assist Gravity turn Hohmann transfer Low energy transfer Oberth effect Inclination change Phasing Rocket equation Rendezvous Transposition, docking, and extraction Orbital mechanics Celestial coordinate system Characteristic energy Escape velocity Ephemeris Equatorial coordinate system Ground track Hill sphere Interplanetary Transport Network Kepler 's laws of planetary motion Lagrangian point n - body problem Orbit equation Orbital state vectors Perturbation Retrograde motion Specific orbital energy Specific relative angular momentum Two - line elements List of orbits Retrieved from `` https://en.wikipedia.org/w/index.php?title=Orbital_eccentricity&oldid=799702593 '' Categories : Orbits Hidden categories : Articles containing Ancient Greek - language text All articles with unsourced statements Articles with unsourced statements from September 2016 All articles with vague or ambiguous time Vague or ambiguous time from September 2016 Use dmy dates from August 2011 Talk Contents About Wikipedia Afrikaans বাংলা Беларуская Català Čeština Deutsch Eesti فارسی Français 한국어 हिन्दी Bahasa Indonesia Italiano Latviešu Lëtzebuergesch Magyar Македонски മലയാളം मराठी Bahasa Melayu Nederlands 日本 語 Norsk Norsk nynorsk Occitan Polski Português Română Русский Scots සිංහල Simple English Slovenčina Slovenščina Српски / srpski Srpskohrvatski / српскохрватски Svenska தமிழ் ไทย Türkçe Українська Tiếng Việt 中文 Edit links This page was last edited on 9 September 2017, at 09 : 44. 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Question: which two planets of our solar system have the most eccentric orbits
Answer: Mercury