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Orbital eccentricity

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(Redirected fromEccentricity (orbit))
Amount by which an orbit deviates from a perfect circle
This article is about eccentricity in astrodynamics. For other uses, seeEccentricity (disambiguation).
An elliptic, parabolic, and hyperbolicKepler orbit:
  Elliptic (eccentricity = 0.7)
  Parabolic (eccentricity = 1)
  Hyperbolic orbit (eccentricity = 1.3)
Elliptic orbit by eccentricity
  0 ·   0.2 ·   0.4 ·   0.6 ·   0.8
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Inastrodynamics, theorbital eccentricity of anastronomical object is adimensionless parameter that determines the amount by which itsorbit around another body deviates from a perfectcircle. A value of 0 is acircular orbit, values between 0 and 1 form anelliptic orbit, 1 is aparabolicescape orbit (or capture orbit), and greater than 1 is ahyperbola. The term derives its name from the parameters ofconic sections, as everyKepler orbit is a conic section. It is normally used for the isolatedtwo-body problem, but extensions exist for objects following arosette orbit through the Galaxy.

Definition

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In atwo-body problem with inverse-square-law force, everyorbit is aKepler orbit. Theeccentricity of this Kepler orbit is anon-negative number that defines its shape.

The eccentricity may take the following values:

The eccentricitye is given by[1]

e=1+ 2 E L2  mrdc α2 {\displaystyle e={\sqrt {1+{\frac {\ 2\ E\ L^{2}\ }{\ m_{\text{rdc}}\ \alpha ^{2}\ }}}}}

whereE is the totalorbital energy,L is theangular momentum,mrdc is thereduced mass, andα{\displaystyle \alpha } the coefficient of the inverse-square lawcentral force such as in the theory ofgravity orelectrostatics inclassical physics:F=αr2{\displaystyle F={\frac {\alpha }{r^{2}}}}(α{\displaystyle \alpha } is negative for an attractive force, positive for a repulsive one; related to theKepler problem)

or in the case of a gravitational force:[2]: 24 e=1+2εh2μ2{\displaystyle e={\sqrt {1+{\frac {2\varepsilon h^{2}}{\mu ^{2}}}}}}

whereε is thespecific orbital energy (total energy divided by the reduced mass),μ thestandard gravitational parameter based on the total mass, andh thespecific relative angular momentum (angular momentum divided by the reduced mass).[2]: 12–17 

For values ofe from0 to just under1 the orbit's shape is an increasingly elongated (or flatter) ellipse; for values ofe just over1 to infinity the orbit is ahyperbola branch making a total turn of  2arccsc(e) , decreasing from 180 to 0 degrees. Here, the total turn is analogous toturning number, but for open curves (an angle covered by velocity vector). Thelimit case between an ellipse and a hyperbola, whene equals1, 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 whilee tends to1 (or in the parabolic case, remains1).

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 \ \arcsin(e)\ } gives the projection angle of a perfect circle to anellipse of eccentricitye. For example, to view the eccentricity of the planet Mercury (e = 0.2056), one must simply calculate theinverse sine to find the projection angle of 11.86 degrees. Then, tilting any circular object by that angle, the apparent ellipse of that object projected to the viewer's eye will be of the same eccentricity.

Etymology

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The word "eccentricity" comes fromMedieval Latineccentricus, derived fromGreekἔκκεντροςekkentros "out of the center", fromἐκ-ek-, "out of" +κέντρονkentron "center". "Eccentric" first appeared in English in 1551, with the definition "...a circle in which the earth, sun. etc. deviates from its center".[citation needed] In 1556, five years later, an adjectival form of the word had developed.

Calculation

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The eccentricity of an orbit can be calculated from theorbital state vectors as themagnitude of theeccentricity vector:e=|e|{\displaystyle e=\left|\mathbf {e} \right|}where:

  • e is the eccentricity vector ("Hamilton's vector").[2]: 25, 62–63 

Forelliptical orbits it can also be calculated from theperiapsis andapoapsis sincerp=a(1e){\displaystyle r_{\text{p}}=a\,(1-e)} andra=a(1+e),{\displaystyle r_{\text{a}}=a\,(1+e)\,,} wherea is the length of thesemi-major axis.e=rarpra+rp=ra/rp1ra/rp+1=12rarp+1{\displaystyle {\begin{aligned}e&={\frac {r_{\text{a}}-r_{\text{p}}}{r_{\text{a}}+r_{\text{p}}}}\\\,\\&={\frac {r_{\text{a}}/r_{\text{p}}-1}{r_{\text{a}}/r_{\text{p}}+1}}\\\,\\&=1-{\frac {2}{\;{\frac {r_{\text{a}}}{r_{\text{p}}}}+1\;}}\end{aligned}}}where:

  • ra is the radius atapoapsis (also "apofocus", "aphelion", "apogee"), i.e., the farthest distance of the orbit to thecenter of mass of the system, which is afocus of the ellipse.
  • rp is the radius atperiapsis (or "perifocus" etc.), the closest distance.

The semi-major axis, a, is also the path-averaged distance to the centre of mass,[2]: 24–25  while the time-averaged distance is a(1 + e e / 2).[1]

The eccentricity of an elliptical orbit can be used to obtain the ratio of theapoapsis radius to theperiapsis radius:rarp=a(1+e)a(1e)=1+e1e{\displaystyle {\frac {r_{\text{a}}}{r_{\text{p}}}}={\frac {\,a\,(1+e)\,}{\,a\,(1-e)\,}}={\frac {1+e}{1-e}}}

For Earth, orbital eccentricitye0.01671,apoapsis is aphelion andperiapsis is perihelion, relative to the Sun.

For Earth's annual orbit path, the ratio of longest radius (ra) / shortest radius (rp) israrp=1+e1e ≈ 1.03399 .{\displaystyle {\frac {\,r_{\text{a}}\,}{r_{\text{p}}}}={\frac {\,1+e\,}{1-e}}{\text{ ≈ 1.03399 .}}}

Examples

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Plot of the changing orbital eccentricities ofMercury,Venus,Earth andMars over the next 50 000 years. The arrows indicate the different scales used, as the eccentricities of Mercury and Mars are much greater than those of Venus and Earth. The 0 point on x-axis in this plot is the year 2007.
Eccentricities of Solar System bodies
ObjectEccentricity
Triton0.00002
Venus0.0068
Neptune0.0086
Earth0.0167
Titan0.0288
Uranus0.0472
Jupiter0.0484
Saturn0.0541
Luna (Moon)0.0549
Ceres0.0758
Vesta0.0887
Mars0.0934
10 Hygiea0.1146
Quaoar0.1500
Makemake0.1559
Haumea0.1887
Mercury0.2056
2 Pallas0.2313
Orcus0.2450
Pluto0.2488
3 Juno0.2555
324 Bamberga0.3400
Eris0.4407
Gonggong0.4500
8405 Asbolus0.5800
5145 Pholus0.6100
944 Hidalgo0.6775
Nereid0.7507
2001 XA2550.7755
5335 Damocles0.8386
Sedna0.8549
Halley's Comet0.9671
Comet Hale-Bopp0.9951
Comet Ikeya-Seki0.9999
Comet McNaught1.0002[a]
C/1980 E11.057
ʻOumuamua1.20[b]
2I/Borisov3.5[c]

The table lists the values for all planets and dwarf planets, and selected asteroids, comets, and moons.Mercury has the greatest orbital eccentricity of any planet in theSolar System (e =0.2056), followed byMars of0.0934. Such eccentricity is sufficient for Mercury to receive twice as muchsolar irradiation at perihelion compared to aphelion. Before its demotion fromplanet status in 2006,Pluto was considered to be the planet with the most eccentric orbit (e =0.248). OtherTrans-Neptunian objects have significant eccentricity, notably the dwarf planetEris (0.44). Even further out,Sedna has an extremely-high eccentricity of0.855 due to its estimated aphelion of 937 AU and perihelion of about 76 AU, possibly under influence ofunknown object(s).

The eccentricity ofEarth's orbit is currently about0.0167; its orbit is nearly circular.Neptune's andVenus's have even lower eccentricities of0.0086 and0.0068 respectively, the latter being the least orbital eccentricity of any planet in the Solar System. Over hundreds of thousands of years, the eccentricity of the Earth's orbit varies from nearly0.0034 to almost 0.058 as a result of gravitational attractions among the planets.[4]

Luna's value is0.0549, the most eccentric of the large moons in the Solar System. The fourGalilean moons (Io,Europa,Ganymede andCallisto) have their eccentricities of less than 0.01.Neptune's largest moonTriton has an eccentricity of1.6×10−5 (0.000016),[5] the smallest eccentricity of any known moon in the Solar System;[citation needed] its orbit is as close to a perfect circle as can be currently[when?] measured. Smaller moons, particularlyirregular moons, can have significant eccentricities, such as Neptune's third largest moon,Nereid, of0.75.

Most of the Solar System'sasteroids have orbital eccentricities between 0 and 0.35 with an average value of 0.17.[6] Their comparatively high eccentricities are probably due to under influence ofJupiter and to past collisions.

Comets have very different values of eccentricities.Periodic comets have eccentricities mostly between 0.2 and 0.7,[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 includeComet Hale–Bopp with a value of0.9951,[8]Comet Ikeya-Seki with a value of0.9999 andComet McNaught (C/2006 P1) with a value of1.000019.[9] As first two's values are less than 1, their orbit are elliptical and they will return.[8] McNaught has ahyperbolic orbit but within the influence of the inner planets,[9] is still bound to the Sun with an orbital period of about 105 years.[3]Comet C/1980 E1 has the largest eccentricity of any known hyperbolic comet of solar origin with an eccentricity of 1.057,[10] and will eventually leave the Solar System.

ʻOumuamua is the firstinterstellar object to be found passing through the Solar System. Its orbital eccentricity of 1.20 indicates that ʻOumuamua has never been gravitationally bound to the Sun. It was discovered 0.2 AU (30000000 km;19000000 mi) from Earth and is roughly 200 meters in diameter. It has an interstellar speed (velocity at infinity) of 26.33 km/s (58900 mph).

TheexoplanetHD 20782 b has the most eccentric orbit known of 0.97 ± 0.01,[11] followed byHD 80606 b of 0.93226+0.00064
−0.00069
.[12]

Mean average

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The mean eccentricity of an object is the average eccentricity as a result ofperturbations over a given time period. Neptune currently has an instant (currentepoch) eccentricity of0.0113,[13] but from 1800 to 2050 has a mean eccentricity of0.00859.[14]

Climatic effect

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Orbital mechanics require that the duration of the seasons be proportional to the area of Earth's orbit swept between thesolstices andequinoxes, 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. Northern hemisphere autumn and winter occur at closest approach (perihelion), when Earth is moving at its maximum velocity—while the opposite occurs in the southern hemisphere. As a result, in the northern hemisphere, autumn 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 autumn due to orbital eccentricity.[15][16]

Apsidal precession also slowly changes the place in Earth's orbit where the solstices and equinoxes occur. This is a slow change in the orbit of Earth, not the axis of rotation, which is referred to asaxial precession. The climatic effects of this change are part of theMilankovitch cycles. Over the next10000 years, the northern hemisphere winters will become gradually longer and summers will become shorter. 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.[17] This will reduce the mean orbital radius and raise temperatures in both hemispheres closer to the mid-interglacial peak.

Exoplanets

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Of the manyexoplanets discovered, most have a higher orbital eccentricity than planets in the Solar System. Exoplanets found with low orbital eccentricity (near-circular orbits) are very close to their star and aretidally-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.[18] 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 othermultiplanetary systems have been found, but none resemble the Solar System. The Solar System has uniqueplanetesimal systems, which led the planets to have near-circular orbits. Solar planetesimal systems include theasteroid belt,Hilda family,Kuiper belt,Hills cloud, and theOort cloud. The exoplanet systems discovered have either no planetesimal systems or a very large one. Low eccentricity is needed for habitability, especially advanced life.[19] High multiplicity planet systems are much more likely to have habitable exoplanets.[20][21] Thegrand tack hypothesis of the Solar System also helps understand its near-circular orbits and other unique features.[22][23][24][25][26][27][28][29]

See also

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Footnotes

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  1. ^While its orbit was initially hyperbolic, it would be bound to the Sun later due to the influence of planets[3]
  2. ^ʻOumuamua was never bound to the Sun, so its orbit is hyperbolic:e ≈ 1.20 > 1
  3. ^C/2019 Q4 (Borisov) was never bound to the Sun, so its orbit is hyperbolic:e ≈ 3.5 > 1

References

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  1. ^Abraham, Ralph (2008).Foundations of Mechanics. Marsden, Jerrold E. (2nd ed.). Providence, RI: AMS Chelsea Pub./American Mathematical Society.ISBN 978-0-8218-4438-0.OCLC 191847156.
  2. ^abcdBate, Roger R.; Mueller, Donald D.; White, Jerry E.; Saylor, William W. (2020).Fundamentals of Astrodynamics.Courier Dover.ISBN 978-0-486-49704-4. Retrieved4 March 2022.
  3. ^ab"McNaught (C/2006 P1): Heliocentric elements 2006–2050". Jet Propulsion Laboratory. 18 July 2007. Retrieved10 November 2018.
  4. ^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). Archived fromthe original on 6 January 2018.
  5. ^David R. Williams (22 January 2008)."Neptunian Satellite Fact Sheet". NASA.
  6. ^AsteroidsArchived 4 March 2007 at theWayback Machine
  7. ^Lewis, John (2 December 2012).Physics and Chemistry of the Solar System. Academic Press.ISBN 9780323145848.
  8. ^ab"JPL Small-Body Database Browser: C/1995 O1 (Hale-Bopp)" (2007-10-22 last obs). Retrieved5 December 2008.
  9. ^ab"JPL Small-Body Database Browser: C/2006 P1 (McNaught)" (2007-07-11 last obs). Retrieved17 December 2009.
  10. ^"JPL Small-Body Database Browser: C/1980 E1 (Bowell)" (1986-12-02 last obs). Retrieved22 March 2010.
  11. ^S. J. O'Toole; C. G. Tinney; H. R. A. Jones; R. P. Butler; G. W. Marcy; B. Carter; J. Bailey (2009)."Selection Functions in Doppler Planet Searches".MNRAS. 392, 641 (2):641–654.arXiv:0810.1589.Bibcode:2009MNRAS.392..641O.doi:10.1111/j.1365-2966.2008.14051.x.S2CID 7248338.
  12. ^"Investigating the Mystery of Migrating 'Hot Jupiters'".Jet Propulsion Laboratory. 28 March 2016.Archived from the original on 24 March 2023.
  13. ^Williams, David R. (29 November 2007)."Neptune Fact Sheet". NASA.
  14. ^"Keplerian elements for 1800 A.D. to 2050 A.D." JPL Solar System Dynamics. Retrieved17 December 2009.
  15. ^Data fromUnited States Naval ObservatoryArchived 13 October 2007 at theWayback Machine
  16. ^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.
  17. ^"Long Term Climate".ircamera.as.arizona.edu. Archived fromthe original on 2 June 2015. Retrieved1 September 2016.
  18. ^"ECCENTRICITY".exoplanets.org.
  19. ^Ward, Peter; Brownlee, Donald (2000).Rare Earth: Why Complex Life is Uncommon in the Universe. Springer. pp. 122–123.ISBN 0-387-98701-0.
  20. ^Limbach, MA; Turner, EL (2015)."Exoplanet orbital eccentricity: multiplicity relation and the Solar System".Proc Natl Acad Sci U S A.112 (1):20–4.arXiv:1404.2552.Bibcode:2015PNAS..112...20L.doi:10.1073/pnas.1406545111.PMC 4291657.PMID 25512527.
  21. ^Youdin, Andrew N.; Rieke, George H. (15 December 2015). "Planetesimals in Debris Disks".arXiv:1512.04996.{{cite journal}}:Cite journal requires|journal= (help)
  22. ^Zubritsky, Elizabeth."Jupiter's Youthful Travels Redefined Solar System".NASA. Archived fromthe original on 9 June 2011. Retrieved4 November 2015.
  23. ^Sanders, Ray (23 August 2011)."How Did Jupiter Shape Our Solar System?".Universe Today. Retrieved4 November 2015.
  24. ^Choi, Charles Q. (23 March 2015)."Jupiter's 'Smashing' Migration May Explain Our Oddball Solar System". Space.com. Retrieved4 November 2015.
  25. ^Davidsson, Dr. Björn J. R. (9 March 2014)."Mysteries of the asteroid belt".The History of the Solar System. Retrieved7 November 2015.
  26. ^Raymond, Sean (2 August 2013)."The Grand Tack".PlanetPlanet. Retrieved7 November 2015.
  27. ^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.arXiv:1407.3290.Bibcode:2014Icar..239...74O.doi:10.1016/j.icarus.2014.05.009.S2CID 51737711.
  28. ^Loeb, Abraham; Batista, Rafael; Sloan, David (August 2016). "Relative Likelihood for Life as a Function of Cosmic Time".Journal of Cosmology and Astroparticle Physics.2016 (8): 040.arXiv:1606.08448.Bibcode:2016JCAP...08..040L.doi:10.1088/1475-7516/2016/08/040.S2CID 118489638.
  29. ^"Is Earthly Life Premature from a Cosmic Perspective?". Harvard-Smithsonian Center for Astrophysics. 1 August 2016.

Further reading

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