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Apsis

Either of two extreme points in a celestial object's orbit


Either of two extreme points in a celestial object's orbit

An apsis ( (third declension); ) is the farthest or nearest point in the orbit of a planetary body about its primary body. The line of apsides (also called apse line, or major axis of the orbit) is the line connecting the two extreme values.

Apsides pertaining to orbits around different bodies have distinct names to differentiate themselves from other apsides. Apsides pertaining to geocentric orbits, orbits around the Earth, are at the farthest point called the apogee, and at the nearest point the perigee, as with orbits of satellites and the Moon around Earth. Apsides pertaining to orbits around the Sun are named aphelion for the farthest and perihelion for the nearest point in a heliocentric orbit. 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.

General description

There are two apsides in any elliptic orbit. The name for each apsis is created from the prefixes ap-, apo- () for the farthest or peri- () for the closest point to the primary body, with a suffix that describes the primary body. The suffix for Earth is -gee, so the apsides' names are apogee and perigee. For the Sun, the suffix is -helion, so the names are aphelion and perihelion.

According to Newton's laws of motion, all periodic orbits are ellipses. The barycenter of the two bodies may lie well within the bigger body—e.g., the Earth–Moon barycenter is about 75% of the way from Earth's center to its surface. If, compared to the larger mass, the smaller mass is negligible (e.g., for satellites), then the orbital parameters are independent of the smaller mass.

When used as a suffix—that is, -apsis—the term can refer to the two distances from the primary body to the orbiting body when the latter is located: 1) at the periapsis point, or 2) at the apoapsis point (compare both graphics, second figure). The line of apsides denotes the distance of the line that joins the nearest and farthest points across an orbit; it also refers simply to the extreme range of an object orbiting a host body (see top figure; see third figure).

In orbital mechanics, the apsides technically refer to the distance measured between the barycenter of the 2-body system and the center of mass of the orbiting body. However, in the case of a spacecraft, the terms are commonly used to refer to the orbital altitude of the spacecraft above the surface of the central body (assuming a constant, standard reference radius).

Terminology

The words "pericenter" and "apocenter" are often seen, although periapsis/apoapsis are preferred in technical usage.

  • For generic situations where the primary is not specified, the terms pericenter and apocenter are used for naming the extreme points of orbits (see table, top figure); periapsis and apoapsis (or apapsis) are equivalent alternatives, but these terms also frequently refer to distances—that is, the smallest and largest distances between the orbiter and its host body (see second figure).
  • For a body orbiting the Sun, the point of least distance is the perihelion (), and the point of greatest distance is the aphelion (); when discussing orbits around other stars the terms become periastron and apastron.
  • When discussing a satellite of Earth, including the Moon, the point of least distance is the perigee (), and of greatest distance, the apogee (from Ancient Greek: Γῆ (), "land" or "earth").
  • For objects in lunar orbit, the point of least distance are called the pericynthion () and the greatest distance the apocynthion (). The terms perilune and apolune, as well as periselene and aposelene are also used. Since the Moon has no natural satellites this only applies to man-made objects.

Etymology

The words perihelion and aphelion were coined by Johannes Kepler to describe the orbital motions of the planets around the Sun. The words are formed from the prefixes peri- (Greek: περί, near) and apo- (Greek: ἀπό, away from), affixed to the Greek word for the Sun, (ἥλιος, or hēlíos).

Various related terms are used for other celestial objects. The suffixes -gee, -helion, -astron and -galacticon are frequently used in the astronomical literature when referring to the Earth, Sun, stars, and the Galactic Center respectively. The suffix -jove is occasionally used for Jupiter, but -saturnium has very rarely been used in the last 50 years for Saturn. The -gee form is also used as a generic closest-approach-to "any planet" term—instead of applying it only to Earth.

During the Apollo program, the terms pericynthion and apocynthion were used when referring to orbiting the Moon; they reference Cynthia, an alternative name for the Greek Moon goddess Artemis. More recently, during the Artemis program, the terms perilune and apolune have been used.

Regarding black holes, the term peribothron was first used in a 1976 paper by J. Frank and M. J. Rees, who credit W. R. Stoeger for suggesting creating a term using the greek word for pit: "bothron". The terms perimelasma and apomelasma (from a Greek root) were used by physicist and science-fiction author Geoffrey A. Landis in a story published in 1998,Perimelasma , by Geoffrey Landis, first published in Asimov's Science Fiction, January 1998, republished at Infinity Plus thus appearing before perinigricon and aponigricon (from Latin) in the scientific literature in 2002.

Terminology summary

The suffixes shown below may be added to prefixes peri- or apo- to form unique names of apsides for the orbiting bodies of the indicated host/(primary) system. However, only for the Earth, Moon and Sun systems are the unique suffixes commonly used. Exoplanet studies commonly use -astron, but typically, for other host systems the generic suffix, -apsis, is used instead.

Astronomical
host objectSuffixOrigin
of the name
SunHelios
MercuryHermes
Venus
Cytherean
EarthGaia
Moon
Luna
Cynthia
Selene
MarsAres
CeresDemeter
JupiterZeus
Jupiter
Saturn
Cronos
Saturn
UranusUranus
Neptune
Poseidon
Astronomical
host objectSuffixOrigin
of the name
Star-astronLat: astra; *stars*
Galaxy-galacticonGr: galaxias; *galaxy*
Barycenter-center
-focus
-apsis
Black hole-melasma
-bothron
-nigriconGr: melos; *black*
Gr: bothros; *hole*
Lat: niger; *black*

Perihelion and aphelion

The perihelion (q) and aphelion (Q) are the nearest and farthest points, respectively, of a body's direct orbit around the Sun.

Comparing osculating elements at a specific epoch to those at a different epoch will generate differences. The time-of-perihelion-passage as one of six osculating elements is not an exact prediction (other than for a generic two-body model) of the actual minimum distance to the Sun using the full dynamical model. Precise predictions of perihelion passage require numerical integration.

Inner planets and outer planets

The two images below show the orbits, orbital nodes, and positions of perihelion (q) and aphelion (Q) for the planets of the Solar System as seen from above the northern pole of Earth's ecliptic plane, which is coplanar with Earth's orbital plane. The planets travel counterclockwise around the Sun and for each planet, the blue part of their orbit travels north of the ecliptic plane, the pink part travels south, and dots mark perihelion (green) and aphelion (orange).

The first image (below-left) features the inner planets, situated outward from the Sun as Mercury, Venus, Earth, and Mars. The reference Earth-orbit is colored yellow and represents the orbital plane of reference. At the time of vernal equinox, the Earth is at the bottom of the figure. The second image (below-right) shows the outer planets, being Jupiter, Saturn, Uranus, and Neptune.

The orbital nodes are the two end points of the "line of nodes" where a planet's tilted orbit intersects the plane of reference; here they may be 'seen' as the points where the blue section of an orbit meets the pink.

Image:Inner Planet Orbits 02.svg|The perihelion (green) and aphelion (orange) points of the inner planets of the Solar System Image:Outer Planet Orbits 02.svg|The perihelion (green) and aphelion (orange) points of the outer planets of the Solar System

Lines of apsides

The chart shows the extreme range—from the closest approach (perihelion) to farthest point (aphelion)—of several orbiting celestial bodies of the Solar System: the planets, the known dwarf planets, including Ceres, and Halley's Comet. The length of the horizontal bars correspond to the extreme range of the orbit of the indicated body around the Sun. These extreme distances (between perihelion and aphelion) are the lines of apsides of the orbits of various objects around a host body.

Earth perihelion and aphelion

In the 21st century, the Earth reaches perihelion in early January, approximately 14 days after the December solstice. At perihelion, the Earth's center is about 0.9833 AU from the Sun's center. In contrast, the Earth reaches aphelion currently in early July, approximately 14 days after the June solstice. The aphelion distance between the Earth's and Sun's centers is currently about 1.01664 AU.{{cite web

The dates of perihelion and aphelion change over a century due to precession and other orbital factors, which follow cyclical patterns known as Milankovitch cycles. In the short-term, such dates can vary up to 3 days from one year to another as with aphelion on 3 July 2025 and 6 July 2026. This short-term variation is due to the presence of the Moon: while the Earth–Moon barycenter is moving on a stable orbit around the Sun, the position of the Earth's center which is on average about 4700 km from the barycenter, could be shifted in any direction from it—and this affects the timing of the actual closest approach between the Sun's and the Earth's centers (which in turn defines the timing of perihelion in a given year). On a longer time scale, the last July 3 aphelion is in 2060, and the last January 2 perihelion is in 2089. The first July 7 aphelion is in 2067.

Because of the increased distance at aphelion, only 93.55% of the radiation from the Sun falls on a given area of Earth's surface as does at perihelion, but this does not account for the seasons, which result instead from the tilt of Earth's axis of 23.4° away from perpendicular to the plane of Earth's orbit. Indeed, at both perihelion and aphelion it is summer in one hemisphere while it is winter in the other one. Winter falls on the hemisphere where sunlight strikes least directly, and summer falls where sunlight strikes most directly, regardless of the Earth's distance from the Sun.

In the northern hemisphere, summer occurs at the same time as aphelion, when solar radiation is lowest. Despite this, summers in the northern hemisphere are on average 2.3 C-change warmer than in the southern hemisphere, because the northern hemisphere contains larger land masses, which are easier to heat than the seas.

Perihelion and aphelion do however have an indirect effect on the seasons: because Earth's orbital speed is minimum at aphelion and maximum at perihelion, the planet takes longer to orbit from June solstice to September equinox than it does from December solstice to March equinox. Therefore, summer in the northern hemisphere lasts slightly longer (93 days) than summer in the southern hemisphere (89 days).

Astronomers commonly express the timing of perihelion relative to the First Point of Aries not in terms of days and hours, but rather as an angle of orbital displacement, the so-called longitude of the periapsis (also called longitude of the pericenter). For the orbit of the Earth, this is called the longitude of perihelion, and in 2000 it was about 282.895°; by 2010, this had advanced by a small fraction of a degree to about 283.067°, i.e. a mean increase of 62" per year.

For the orbit of the Earth around the Sun, the time of apsis is often expressed in terms of a time relative to seasons, since this determines the contribution of the elliptical orbit to seasonal variations. The variation of the seasons is primarily controlled by the annual cycle of the elevation angle of the Sun, which is a result of the tilt of the axis of the Earth measured from the plane of the ecliptic. The Earth's eccentricity and other orbital elements are not constant, but vary slowly due to the perturbing effects of the planets and other objects in the solar system (Milankovitch cycles).

On a very long time scale, the dates of perihelion and of aphelion progress through the seasons, and they make one complete cycle in 22,000 to 26,000 years. By the year 3800, perihelion will regularly occur in February.

YearPerihelionAphelionDateTime (UT)DateTime (UT)201020112012201320142015201620172018201920202021202220232024202520262027202820292030203120322033203420353800
January 300:09July 611:30
January 318:32July 414:54
January 500:32July 503:32
January 204:38July 514:44
January 411:59July 400:13
January 406:36July 619:40
January 222:49July 416:24
January 414:18July 320:11
January 305:35July 616:47
January 305:20July 422:11
January 507:48July 411:35
January 213:51July 522:27
January 406:55July 407:11
January 416:17July 620:07
January 300:39July 505:06
January 413:28July 319:55
January 317:16July 617:31
January 302:33July 505:06
January 512:28July 322:18
January 218:13July 605:12
January 310:12July 412:58
January 420:48July 607:10
January 305:11July 511:54
January 411:51July 320:52
January 404:47July 618:49
January 300:54July 518:22
February 2August 4

Other planets

The following table shows the distances of the planets and dwarf planets from the Sun at their perihelion and aphelion.

Type of bodyBodyDistance from Sun at perihelionDistance from Sun at aphelionDifference (%){\text{aphelion distance}}}}Insolation
difference (%){\text{aphelion distance}}\right)^2}}(km)(miles)(km)(miles)
Planet46001009 km69817445 km34.1%56.6%
107476170 km108942780 km1.3%2.7%
147098291 km152098233 km3.3%6.5%
206655215 km249232432 km17.1%31.2%
740679835 km816001807 km9.2%17.6%
1349823615 km1503509229 km10.2%19.4%
2734998229 km3006318143 km9.0%17.2%
4459753056 km4537039826 km1.7%3.4%
Dwarf planet380951528 km446428973 km14.7%27.2%
4436756954 km7376124302 km39.8%63.8%
5157623774 km7706399149 km33.1%55.2%
5671928586 km7894762625 km28.2%48.4%
5765732799 km14594512904 km60.5%84.4%

Mathematical formulae

These formulae characterize the pericenter and apocenter of an orbit: ; Pericenter: Maximum speed, v_\text{per} = \sqrt{ \frac{(1 + e)\mu}{(1 - e)a} } ,, at minimum (pericenter) distance, r_\text{per} = (1 - e)a. ; Apocenter: Minimum speed, v_\text{ap} = \sqrt{\frac{(1 - e)\mu}{(1 + e)a} } ,, at maximum (apocenter) distance, r_\text{ap} = (1 + e)a.

While, in accordance with Kepler's laws of planetary motion (based on the conservation of angular momentum) and the conservation of energy, these two quantities are constant for a given orbit: ; Specific relative angular momentum: h = \sqrt{\left(1 - e^2\right)\mu a} ; Specific orbital energy: \varepsilon = -\frac{\mu}{2a}

where:

  • r_\text{ap} is the distance from the apocenter to the primary focus
  • r_\text{per} is the distance from the pericenter to the primary focus
  • a is the semi-major axis:
  • : a = \frac{r_\text{per} + r_\text{ap}}{2}
  • μ is the standard gravitational parameter
  • e is the eccentricity, defined as
  • : e = \frac{r_\text{ap} - r_\text{per}}{r_\text{ap} + r_\text{per}} = 1 - \frac{2}{\frac{r_\text{ap}}{r_\text{per}} + 1}

Note that for conversion from heights above the surface to distances between an orbit and its primary, the radius of the central body has to be added, and conversely.

The arithmetic mean of the two limiting distances is the length of the semi-major axis a. The geometric mean of the two distances is the length of the semi-minor axis b.

The geometric mean of the two limiting speeds is :\sqrt{-2\varepsilon} = \sqrt{\frac{\mu}{a}}

which is the speed of a body in a circular orbit whose radius is a.

Time of perihelion

Orbital elements such as the time of perihelion passage are defined at the epoch chosen using an unperturbed two-body solution that does not account for the n-body problem. To get an accurate time of perihelion passage you need to use an epoch close to the perihelion passage. For example, using an epoch of 1996, Comet Hale–Bopp shows perihelion on 1 April 1997. Using an epoch of 2022 shows a less accurate perihelion date of 29 March 1997. Short-period comets can be even more sensitive to the epoch selected. Using an epoch of 2005 shows 101P/Chernykh coming to perihelion on 25 December 2005, but using an epoch of 2012 produces a less accurate unperturbed perihelion date of 20 January 2006.

12P

EpochDate of perihelion (tp)
[2010](https://archive.today/20220623124113/https://ssd.jpl.nasa.gov/tools/sbdb_lookup.html%23/?sstr=12P&view=OPC)2024-Apr-19.892
n-body{{cite webtitle=Horizons Batch for 12P/Pons-Brooks (90000223) at 2024-Apr-21
[2018](https://archive.today/20230211111847/https://ssd.jpl.nasa.gov/tools/sbdb_lookup.html%23/?sstr=12P&view=OPC)2024-Apr-23.069

Numerical integration shows dwarf planet Eris will come to perihelion around December 2257.{{cite web |access-date = 13 September 2021 |archive-date = September 13, 2021 |archive-url = https://web.archive.org/web/20210913110143/https://ssd.jpl.nasa.gov/horizons_batch.cgi?batch=1&COMMAND=%27Eris%27&START_TIME=%272257-11-28%27&STOP_TIME=%272257-12-17%27&STEP_SIZE=%273%20hours%27&QUANTITIES=%2719%27 |url-status = live

4 Vesta came to perihelion on 26 December 2021,{{cite web |access-date=2021-09-26 |archive-date=September 26, 2021 |archive-url=https://web.archive.org/web/20210926095954/https://ssd.jpl.nasa.gov/horizons_batch.cgi?batch=1&COMMAND=%27Vesta%27&START_TIME=%272021-Dec-25%2023%3A00%27&STOP_TIME=%272021-Dec-26%2004%3A00%27&STEP_SIZE=%2715%20minutes%27&QUANTITIES=%2719%27 |url-status=live

Short observation periods

Trans-Neptunian objects that are discovered when they are more than 80 AU from the Sun present a major challenge for astronomers. Because these objects move extremely slowly across the sky, scientists need many observations taken over several years to accurately determine their orbital paths.

When astronomers have only limited data—like when there were only 8 observations of object collected over just one year—the uncertainty becomes enormous. For objects that won’t reach their closest point to the Sun (perihelion) for roughly 100 years, this limited data can lead to massive uncertainties. In the case of , scientists originally estimated the perihelion date could be off by plus or minus 28220 day (a 1-sigma uncertainty) —that’s nearly an entire human lifetime of uncertainty.

This demonstrates why tracking these distant objects requires patience and long-term observation campaigns to pin down their true orbital characteristics.

References

References

  1. {{cite Dictionary.com. apsis
  2. {{cite American Heritage Dictionary. apsis
  3. (2023-07-06). "Happy Aphelion Day! Earth is at its farthest from the sun for 2023 today".
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  5. Since the Sun, Ἥλιος in Greek, begins with a vowel (H is the long ē vowel in Greek), the final o in "apo" is omitted from the prefix. The pronunciation "Ap-helion" is given in many dictionaries [https://www.oxforddictionaries.com/definition/english/aphelion] {{Webarchive. link. (December 22, 2015, pronouncing the "p" and "h" in separate syllables. However, the pronunciation {{IPAc-en). ə. ˈ. f. iː. l. i. ə. n [http://www.dictionary.com/browse/aphelion] {{Webarchive. link. (July 29, 2017 is also common (''e.g.,'' ''McGraw Hill Dictionary of Scientific and Technical Terms,'' 5th edition, 1994, p. 114), since in late Greek, 'p' from ἀπό followed by the 'h' from ἥλιος becomes phi; thus, the Greek word is αφήλιον. (see, for example, Walker, John, ''A Key to the Classical Pronunciation of Greek, Latin, and Scripture Proper Names'', Townsend Young 1859 [https://play.google.com/store/books/details?id=LuF-9HKGbl4C&rdid=book-LuF-9HKGbl4C&rdot=1] {{Webarchive). link. (September 21, 2019, page 26.) Many [https://www.merriam-webster.com/dictionary/aphelion] dictionaries give both pronunciations)
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