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Jet Propulsion Laboratory Development Ephemeris

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was created in June 2020. The new DE440 / 441 general-purpose planetary solution includes seven additional years of ground and space-based astrometric data, data calibrations, and dynamical model improvements, most significantly involving Jupiter, Saturn, Pluto, and the Kuiper Belt. Inclusion of
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as data files containing the Chebyshev coefficients, along with source code to recover (calculate) positions and velocities. Files vary in the time periods they cover, ranging from a few hundred years to several thousand, and bodies they include. Data may be based on each planet's geometric center or
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Note that these precision numbers are for the interpolated values relative to the original tabulated coordinates. The overall precision and accuracy of interpolated values for describing the actual motions of the planets will be a function of both the precision of the ephemeris tabulated coordinates
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was released with DE405 in 1998. A Long Ephemeris, this was the condensed version of DE405, covering 3000 BC to AD 3000 with the same limitations as DE404. This is the same integration as DE405, with the accuracy of the interpolating polynomials has been lessened to reduce file size for the longer
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spacecraft, the latest estimates of planetary masses, additional lunar laser ranging, and two more months of CCD measurements of Pluto. When initially released in 2008, the DE421 ephemeris covered the years 1900 to 2050. An additional data release in 2013 extended the coverage to the year 2200.
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spacecraft was included in the fit, improving the orbit of Saturn, but rigorous analysis of the data was deferred to a later date. DE418 covered the years 1899 to 2051, and JPL recommended not using it outside of that range due to minor inconsistencies which remained in the planets' masses due to
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JPL uses the ephemerides for navigation of spacecraft throughout the Solar System. Typically, a new ephemeris is computed including the latest available observations of the target planet(s), either for planning of the mission(s), or for final contact of the spacecraft with the target. See below,
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was created in 2013 and is intended for analysis of earlier historical observations of the Sun, Moon, and planets. It covers a longer time span than DE430 (13201 BC to AD 17191) agreeing with DE430 within 1 meter over the time period covered by DE430. Position of the Moon is accurate within 20
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spacecraft at Jupiter, in particular). The method of modeling the asteroids' perturbations was improved, although the same number of asteroids were modeled. The ephemeris was more accurately oriented onto the ICRF. DE405 covered 1600 to 2200 to full precision. This ephemeris was utilized in the
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relative to DE430. The 114 Megabyte ephemeris files include the orientation of the Moon. It spans the years 1550–2650. JPL started transitioning to DE440 in early April 2021. Supplemental versions are also available which include the planetary geometric center of Mars as well as Mars'
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star catalog, were included in the fit. Mars spacecraft ranging and VLBI observations were updated through 2007. Asteroid masses were estimated differently. Lunar laser ranging data for the Moon was added for the first time since DE403, significantly improving the lunar orbit and librations.
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Software is available to use the JPL ephemerides for the production of apparent ephemerides for any location and time; these are widely used by professional and amateur astronomers for reducing planetary observations and producing very precise observing
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was released in 1996. A so-called Long Ephemeris, this condensed version of DE403 covered 3000 BC to AD 3000. While both DE403 and DE404 were integrated over the same timespan, the interpolation of DE404 was somewhat reduced in accuracy and
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of 300 asteroids were included, vs DE118/DE200 which included only the five asteroids determined to cause the largest perturbations. Better values of the planets' masses had been found since DE118/DE200, further refining the perturbations.
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was created in June 2020. This ephemeris is longer than DE440, -13,200 to 17,191, but less accurate (due to neglecting lunar core-mantle damping). It is useful for analyzing historical observations that are outside the span of DE440.
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was also released in 2003 covered 1901 - 2019, with improvements from DE409 in the masses for Venus, Mars, Jupiter, Saturn and the Earth-Moon system based on recent research. Though the masses had not yet been adopted by the
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was created in 2013 and Is intended for use in analyzing modern data. It covers the dates 1550 January 1 to 2650 January 22 with the most accurate lunar ephemeris. From 2015 onwards this ephemeris is utilized in the
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to modern, relativistic theory. From 1975 through 1982, six ephemerides were produced at JPL using the modern techniques of least-squares adjustment of numerically-integrated output to high precision data:
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spacecraft were reprocessed to give data points for Saturn. These resulted in improvements over DE405, especially to the predicted positions of Mars and Saturn. DE409 covered the years 1901 to 2019.
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In the days before personal computers, computers were large and expensive, and numerical integrations such as these were run by large organizations with ample resources. The JPL ephemerides prior to
567:(IERS) reference frame, essentially the ICRF. The data compiled by JPL to derive the ephemeris began to move away from limited-accuracy telescopic observations and more toward higher-accuracy 539:
was created in 1981; includes nutations but not librations. Referred to the dynamical equator and equinox of 2000. Covers late 1599 AD through early 2169 AD. This ephemeris was used for the
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was created April 2014. It includes librations but no nutations. DE432 is a minor update to DE430, and is intended primarily to aid the New Horizons project targeting of Pluto.
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ephemeris gives an interpolating precision (relative to the full ephemeris values) no worse than 25 metres for any planet and no worse than 1 metre for the Moon.
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spacecraft were extended to 2005, and further CCD observations of the five outer planets were included in the fit. Some data was accidentally left out of the fit, namely
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was announced in 1969 to be the third release of the JPL Ephemeris Tapes, and was a special purpose, short-duration ephemeris. The then-current JPL Export Ephemeris was
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was the first numerically integrated so-called Long Ephemeris, covering much of history for which useful astronomical observations were available: 1141 BC to AD 3001.
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Newhall, X. X.; Standish, E. M.; Williams, J. G. (1983). "DE 102 - A numerically integrated ephemeris of the moon and planets spanning forty-four centuries".
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was created in 1981; includes nutations but not librations. Referred to the dynamical equator and equinox of 1950. Covers early 1410 BC through late 3002 AD.
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The observational data in the fits has been an evolving set, including: ranges (distances) to planets measured by radio signals from spacecraft, direct
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with ephemerides (data files), source code (for access and basic processing of the data to recover positions and velocities), and documentation.
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with ephemerides (data files), source code (for access and basic processing of the data to recover positions and velocities), and documentation.
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meters between 1913-2113 and that error grows quadratically outside of that range. It is the largest of the ephemerides files at 3.4 gigabytes.
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was created in 1987; includes nutations and librations. Referred to the dynamical equator and equinox of 2000. Covers late 1899 through 2049.
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Standish, E. M. Jr. (July 1990). "The observational basis for JPL's DE 200, the planetary ephemerides of the Astronomical Almanac".
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technique was used to perform the fitting. As of DE421, perturbations from 343 asteroids, representing about 90% of the mass of the
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Standish; Newhall; Williams; Yeomans (1992), "CHAPTER 5: Orbital Ephemerides of the Sun, Moon, and Planets", in Seidelmann (ed.),
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spacecraft and additional range and VLBI data from the Venus Express spacecraft were fit. DE423 covered the years 1799 to 2200.
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were published in 2021, with improvements in the orbits of Jupiter, Saturn and Pluto from more recent spacecraft observations.
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In the 1970s and early 1980s, much work was done in the astronomical community to update the astronomical almanacs from the
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was released in 2008. It included additional ranging and VLBI measurements of Mars spacecraft, new ranging and VLBI of the
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was released in 1998. It added several years' extra data from telescopic, radar, spacecraft, and VLBI observations (of the
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30 new Kuiper-belt masses, and the Kuiper Belt ring mass, results in a time-varying shift of ~100 km in DE440's
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Positions and velocities of the Sun, Earth, Moon, and planets, along with the orientation of the Moon, are stored as
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of major Solar System bodies, tabulated at equally spaced intervals of time, covering a specified span of years.
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accuracy was improved, giving better positions of the Moon. DE403 covered the time span early 1599 to mid 2199.
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Peale, S. J.; Yseboodt, M.; Margot, J.-L. (2006). "Long-period forcing of Mercury's libration in longitude".
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The use of Chebyshev polynomials enables highly precise, efficient calculations for any given point in time.
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could no longer be applied to a high enough accuracy to adequately reproduce the observations. The method of
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was created in 2016 and was based on the DE430, with improved orbital data for Jupiter specifically for the
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Standish, E. M. Jr.; Newhall, X. X. (1996). "New accuracy levels for solar system ephemerides (Lecture)".
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mission to Mercury. A Long Ephemeris, it was intended to replace DE406, covering 3000 BC to AD 3000.
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was an unreleased ephemeris, created in 2005 as a longer version of DE406, covering 20,000 years.
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telescopic observations of Pluto in order to give improved positions of the planet and its moon.
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was created in 2018 and was based on the DE430, with improved orbital data for Mercury (for the
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The JPL ephemerides are widely used for planetary science; some examples are included in the
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fit in 32 day-long segments. The ephemerides are now available via World Wide Web and
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JPL ephemerides have been the basis of the ephemerides of sun, moon and planets in the
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Venus data for 1992-94 and Galileo Jupiter data for 1996-97. Some ranging data to the
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Park, Ryan S.; Folkner, William M.; Williams, James G.; Boggs, Dale H. (2021-02-08).
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Ephemerides for Solar System bodies are available through a JPL website and via FTP.
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was used to derive the Earth/Moon mass ratio. DE414 covered the years 1599 to 2201.
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for the new almanacs starting in 1984. DE402 introduced coordinates referred to the
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was widely cited in the astronomical community, but not publicly released by JPL
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was widely cited in the astronomical community, but not publicly released by JPL
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See Astronomical Almanac volumes available through Hathitrust's catalog page at
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The time argument of the JPL integrated ephemerides, in early versions known as
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Park, Ryan S.; Folkner, William M.; Williams, James G.; Boggs, Dale H. (2021).
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mission to Pluto. New observations of Pluto, which took advantage of the new
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was apparently unreleased. Details in readily-available sources are sketchy.
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spacecraft) and telescopic data were included in the fit. The orbits of the
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was created 1993, released in 1995, expressed in the coordinates of the
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of planets, two-dimensional position fixes (on the plane of the sky) by
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Information about JPL ephemerides and links to programs and source code
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at NASA's Navigation and Ancillary Information Facility website and
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since the volumes for 1984 through 2002, which used JPL's ephemeris
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Java source code that implements JPL ephemerides and other theories
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scale, as is necessary in precise work to account for the small
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arrival at Saturn. Further spacecraft ranging and VLBI (to the
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NRAO description of the format and uses of the JPL ephemerides
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Recent ephemerides can be used with the planetarium software
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CHAPTER 8: Orbital Ephemerides of the Sun, Moon, and Planets
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was released in 1995, and was quickly superseded by DE403.
2124:(1 ed.), Mill Valley, CA: University Science Books, 1405:"The JPL planetary and lunar ephemerides DE440 and DE441" 1116:"The JPL Planetary and Lunar Ephemerides DE440 and DE441" 319:
telescopic observations of planets and small bodies, and
1297:"JPL Planetary and Lunar Ephemerides Export Information" 210:. (From 2003 through 2014 the basis was updated to use 1216:"The Planetary and Lunar Ephemerides, DE430 and DE431" 1186:
See US Naval Observatory (Naval Oceanography Portal),
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was applied, using numerical integration to solve the
1940:"Planetary and Lunar Ephemerides, Export Information" 27:(number)) designates one of a series of mathematical 2150:
an unpublished, updated version of the above source.
1306:. 6 December 2005. file "README.txt". Archived from 2055:
IAU's Papers and Information Related to Ephemerides
2121:Explanatory Supplement to the Astronomical Almanac 2095:US Naval Observatory (Naval Oceanography Portal), 1545:"JPL Planetary and Lunar Ephemerides, DE405/LE405" 1470:"JPL Planetary and Lunar Ephemerides, DE403/LE403" 1249:for a good summary of spacecraft radio-navigation. 448:for 1984 through 2002 were based on JPL ephemeris 405:(equivalent to about 1 km at the distance of 2045:Folkner's descriptions of most of JPL's DE series 1011:; see also Newhall, Standish and Williams (1983). 571:of the planets, radio-ranging of spacecraft, and 831:was released in 2010. Position estimates of the 331:, for instance, was fit to 48,479 observations. 1172:https://catalog.hathitrust.org/Record/000635721 714:was released in 2004 with updated ephemeris of 17:Jet Propulsion Laboratory Development Ephemeris 736:was created in 2005 and released in 2006. The 436: 292:of the Earth, the accelerations caused by the 1639:which states that DE408 covered 20,000 years. 273:, have been included in the dynamical model. 8: 290:accelerations caused by the tidal distortion 1873:JPL Interoffice Memorandum IOM 343.R-10-001 1832:JPL Interoffice Memorandum IOM 343.R-08-003 1810:JPL Interoffice Memorandum IOM 343.R-07-005 1788:JPL Interoffice Memorandum IOM 343.R-06-002 1691: 1689: 1680:JPL Interoffice Memorandum IOM 312.N-03-009 1658:JPL Interoffice Memorandum IOM 312.N-03-007 98:. These early releases were distributed on 1825:"The Planetary and Lunar Ephemeris DE421" 1738: 1706:JPL Interoffice Memorandum IOM 343-04-008 1477:JPL Interoffice Memorandum IOM 314.10-127 1430: 1322:"The Astronomical Almanac - Contributors" 1139: 1043: 1041: 1039: 472: 1900: 1898: 425:and the precision of the interpolation. 401:"recovers" accuracy of about 0.001  276:The physics modeled included the mutual 2091:describing features of the ephemerides. 1710:which compares DE413 output with DE411. 1595:which mentions DE407 only very briefly. 1552:JPL Interoffice Memorandum 312.F-98-048 945:"Reading Ephemeris Subsystem SPK Files" 936: 187:International Celestial Reference Frame 1214:Folkner, William (February 15, 2014). 1182: 1180: 782:was released in 2007 for planning the 280:gravitational accelerations and their 2097:"History of the Astronomical Almanac" 1803:"Planetary and Lunar Ephemeris DE418" 1398: 1396: 1299:. 12 October 2007. file "README.txt". 1290: 1288: 1286: 1284: 1209: 1207: 1205: 1203: 1188:"History of the Astronomical Almanac" 984:"JPL Development Ephemeris Number 69" 968:"JPL Development Ephemeris Number 28" 726:on 11 Jul 2005. DE413 was fit to new 214:, and further updated from 2015 when 86:There have been many versions of the 7: 565:International Earth Rotation Service 74:, and geocentric coordinates of the 2075:Matlab code to read the ephemerides 999:JPL Development Ephemeris number 96 841:was created in 2011 to support the 645:spacecraft arrival at Mars and the 296:and Moon, and a model of the lunar 573:very-long-baseline-interferometric 365:became essentially equivalent to T 286:Einstein-Infeld-Hoffmann equations 14: 1727:The Astrophysical Journal Letters 1074:See Standish and Williams in the 797:Estimated position data from the 772:spacecraft orbiting the asteroid 379:Chebyshev polynomial coefficients 1998:"JPL Memorandum IOM 392R-14-003" 1030:NASA MSC Internal Note 71-FM-291 437:Recent ephemerides in the series 1781:"JPL Planetary Ephemeris DE414" 1699:"The Ephemeris of Pluto: DE413" 1673:"JPL Planetary Ephemeris DE410" 1651:"JPL Planetary Ephemeris DE409" 982:O'Handley; et al. (1969). 623:time span covered by the file. 599:of the Moon were not included. 413:it is generally about 0.1  1721:Champion; et al. (2010). 1468:Standish; et al. (1995). 997:Standish; et al. (1976). 1: 1823:Folkner; et al. (2008). 1801:Folkner; et al. (2007). 641:was released in 2003 for the 142:theoretical work of the 1890s 2179:Dynamics of the Solar System 1892:file at the JPL FTP website. 1757:10.1088/2041-8205/720/2/L201 1635:10.1016/j.icarus.2006.10.028 1233:Thornton and Border (2000). 991:JPL Technical Report 32-1465 972:JPL Technical Report 32-1206 902:Mars Reconnaissance Orbiters 819:was created in 2009 for the 740:software was updated to use 452:, and from 2003 to 2014 the 343:relativistic coordinate time 1978:. Jet Propulsion Laboratory 722:of a star by its satellite 456:was based on JPL ephemeris 403:seconds of arc (arcseconds) 327:on the Moon, among others. 2195: 2106:(accessed September 2017). 1938:Folkner (April 30, 2014). 1089:Astronomy and Astrophysics 1050:Astronomy and Astrophysics 2089:JPL Interoffice Memoranda 2060:JPL Solar System Dynamics 1574:"IERS Annual Report 2004" 1377:"Public FTP File Browser" 921:Jet Propulsion Laboratory 491:Ephemerides in the series 417:. The 'reduced accuracy' 341:, became recognized as a 37:Jet Propulsion Laboratory 1432:10.3847/1538-3881/abd414 1410:The Astronomical Journal 1359:"HORIZONS Web-Interface" 1141:10.3847/1538-3881/abd414 1120:The Astronomical Journal 361:'s 2006 redefinition of 284:(a modified form of the 282:relativistic corrections 1958:"JPL Ephemerides Files" 1769:which references DE412. 1455:"JPL Ephemeris READ ME" 1258:See sources cited at ]. 1101:1990A&A...233..252S 1062:1983A&A...125..150N 843:Mars Science Laboratory 179:J2000.0 reference frame 60:rectangular coordinates 2015:"de436s release notes" 752:. Ranging data to the 643:Mars Exploration Rover 616:from 2003 until 2014. 2029:"DE438 release notes" 1561:on February 20, 2012. 1301:Also available is an 926:Fundamental ephemeris 738:numerical integration 248:special perturbations 244:general perturbations 232:numerical integration 183:fundamental ephemeris 181:, was adopted as the 109:were integrated on a 2140:Standish; Williams, 1913:on January 16, 2014. 1853:on January 15, 2012. 1310:on January 15, 2012. 932:Notes and references 904:), and Jupiter (for 854:Astronomical Almanac 754:Mars Global Surveyor 653:Mars Global Surveyor 614:Astronomical Almanac 542:Astronomical Almanac 473:Notes and References 454:Astronomical Almanac 445:Astronomical Almanac 397:calculation for the 203:Astronomical Almanac 129:was integrated on a 41:Pasadena, California 23:(number), or simply 2169:Celestial mechanics 1749:2010ApJ...720L.201C 1719:See, for instance, 1695:See, for instance, 1627:2007Icar..187..365P 1571:See, for instance, 1530:1996IAUS..172...29S 1486:on August 11, 2011. 1423:2021AJ....161..105P 1132:2021AJ....161..105P 1007:1976jden.book.....S 750:equations of motion 742:quadruple-precision 582:Lunar Laser Ranging 545:from 1984 to 2003. 460:. As of 2022, the 386:a planetary-system 294:figure of the Earth 236:equations of motion 218:began to be used.) 135:quadruple precision 2102:2009-03-05 at the 1193:2009-03-05 at the 964:See, for example, 802:time constraints. 718:in support of the 271:main asteroid belt 161:in Sep. 1981, and 2174:Dynamical systems 2131:978-0-935702-68-2 2003:. April 30, 2014. 1927:. April 30, 2014. 1779:Standish (2006). 1697:Standish (2004). 1671:Standish (2003). 1649:Standish (2003). 1543:Standish (1998). 894:), Mars (for the 595:of the Earth and 2186: 2149: 2148: 2136: 2134: 2092: 2084: 2033: 2032: 2025: 2019: 2018: 2011: 2005: 2004: 2002: 1994: 1988: 1987: 1985: 1983: 1972: 1966: 1965: 1960:. Archived from 1954: 1948: 1947: 1935: 1929: 1928: 1921: 1915: 1914: 1909:. Archived from 1902: 1893: 1891: 1886:Folkner (2011). 1883: 1877: 1876: 1870: 1864:Folkner (2010). 1861: 1855: 1854: 1849:. Archived from 1845:Folkner (2011). 1842: 1836: 1835: 1829: 1820: 1814: 1813: 1807: 1798: 1792: 1791: 1785: 1776: 1770: 1768: 1742: 1733:(2): L201–L205. 1717: 1711: 1709: 1703: 1693: 1684: 1683: 1677: 1668: 1662: 1661: 1655: 1646: 1640: 1638: 1610: 1602: 1596: 1594: 1592: 1591: 1585: 1579:. Archived from 1578: 1569: 1563: 1562: 1560: 1554:. Archived from 1549: 1540: 1534: 1533: 1513: 1507: 1506: 1501:. Archived from 1497:Folkner (2011). 1494: 1488: 1487: 1485: 1479:. Archived from 1474: 1465: 1459: 1458: 1451: 1445: 1444: 1434: 1400: 1391: 1390: 1388: 1387: 1381:ssd.jpl.nasa.gov 1373: 1367: 1366: 1355: 1349: 1342: 1336: 1335: 1333: 1331: 1326: 1318: 1312: 1311: 1300: 1292: 1279: 1277: 1272:. Archived from 1265: 1259: 1256: 1250: 1248: 1246: 1240:. Archived from 1239: 1229: 1223: 1222: 1220: 1211: 1198: 1184: 1175: 1168: 1162: 1161: 1143: 1111: 1105: 1104: 1084: 1078: 1072: 1066: 1065: 1045: 1034: 1033: 1027: 1018: 1012: 1010: 994: 988: 979: 974:. Archived from 962: 956: 955: 949: 941: 792:accuracy of the 464:is derived from 259:planetary masses 230:was produced by 177:migrated to the 117:. For instance, 115:double precision 35:produced at the 2194: 2193: 2189: 2188: 2187: 2185: 2184: 2183: 2154: 2153: 2146: 2139: 2132: 2117: 2116: 2113: 2104:Wayback Machine 2087: 2079: 2041: 2036: 2027: 2026: 2022: 2013: 2012: 2008: 2000: 1996: 1995: 1991: 1981: 1979: 1974: 1973: 1969: 1956: 1955: 1951: 1937: 1936: 1932: 1923: 1922: 1918: 1904: 1903: 1896: 1885: 1884: 1880: 1868: 1863: 1862: 1858: 1844: 1843: 1839: 1827: 1822: 1821: 1817: 1805: 1800: 1799: 1795: 1783: 1778: 1777: 1773: 1720: 1718: 1714: 1701: 1696: 1694: 1687: 1675: 1670: 1669: 1665: 1653: 1648: 1647: 1643: 1612: 1605: 1603: 1599: 1589: 1587: 1583: 1576: 1572: 1570: 1566: 1558: 1547: 1542: 1541: 1537: 1515: 1514: 1510: 1496: 1495: 1491: 1483: 1472: 1467: 1466: 1462: 1453: 1452: 1448: 1402: 1401: 1394: 1385: 1383: 1375: 1374: 1370: 1357: 1356: 1352: 1343: 1339: 1329: 1327: 1324: 1320: 1319: 1315: 1304:"older version" 1302: 1295: 1293: 1282: 1276:on 27 May 2019. 1268: 1266: 1262: 1257: 1253: 1244: 1237: 1232: 1230: 1226: 1218: 1213: 1212: 1201: 1195:Wayback Machine 1185: 1178: 1169: 1165: 1113: 1112: 1108: 1086: 1085: 1081: 1073: 1069: 1047: 1046: 1037: 1025: 1020: 1019: 1015: 996: 986: 981: 966:Lieske (1967). 965: 963: 959: 947: 943: 942: 938: 934: 917: 658:Mars Pathfinder 528: 501: 499:Latest releases 493: 431: 375: 368: 339: 325:retroreflectors 311:of spacecraft, 224: 173:, a version of 84: 78:are tabulated. 12: 11: 5: 2192: 2190: 2182: 2181: 2176: 2171: 2166: 2156: 2155: 2152: 2151: 2137: 2130: 2112: 2109: 2108: 2107: 2093: 2085: 2077: 2072: 2067: 2062: 2057: 2052: 2047: 2040: 2039:External links 2037: 2035: 2034: 2020: 2006: 1989: 1967: 1964:on 2019-05-25. 1949: 1930: 1916: 1905:Acton (2013). 1894: 1878: 1856: 1837: 1815: 1793: 1771: 1712: 1685: 1663: 1641: 1621:(2): 365–373. 1597: 1564: 1535: 1508: 1505:on 2012-01-15. 1489: 1460: 1446: 1392: 1368: 1350: 1337: 1313: 1280: 1270:"JPL FTP site" 1260: 1251: 1247:on 2012-02-18. 1224: 1199: 1176: 1163: 1106: 1079: 1067: 1035: 1013: 978:on 2015-01-06. 957: 935: 933: 930: 929: 928: 923: 916: 913: 770:NEAR Shoemaker 527: 524: 500: 497: 492: 489: 488: 487: 480: 476: 469: 440: 430: 427: 374: 371: 366: 337: 223: 220: 153:in Sep. 1977, 149:in Nov. 1975, 123:Univac 1100/81 83: 80: 66:, eight major 13: 10: 9: 6: 4: 3: 2: 2191: 2180: 2177: 2175: 2172: 2170: 2167: 2165: 2162: 2161: 2159: 2145: 2144: 2138: 2133: 2127: 2123: 2122: 2115: 2114: 2110: 2105: 2101: 2098: 2094: 2090: 2086: 2082: 2078: 2076: 2073: 2071: 2068: 2066: 2063: 2061: 2058: 2056: 2053: 2051: 2048: 2046: 2043: 2042: 2038: 2030: 2024: 2021: 2016: 2010: 2007: 1999: 1993: 1990: 1977: 1976:"Ephemerides" 1971: 1968: 1963: 1959: 1953: 1950: 1945: 1941: 1934: 1931: 1926: 1920: 1917: 1912: 1908: 1901: 1899: 1895: 1889: 1882: 1879: 1874: 1867: 1860: 1857: 1852: 1848: 1841: 1838: 1833: 1826: 1819: 1816: 1811: 1804: 1797: 1794: 1789: 1782: 1775: 1772: 1766: 1762: 1758: 1754: 1750: 1746: 1741: 1736: 1732: 1728: 1724: 1716: 1713: 1707: 1700: 1692: 1690: 1686: 1681: 1674: 1667: 1664: 1659: 1652: 1645: 1642: 1636: 1632: 1628: 1624: 1620: 1616: 1608: 1601: 1598: 1586:on 2012-04-26 1582: 1575: 1568: 1565: 1557: 1553: 1546: 1539: 1536: 1531: 1527: 1523: 1519: 1512: 1509: 1504: 1500: 1493: 1490: 1482: 1478: 1471: 1464: 1461: 1456: 1450: 1447: 1442: 1438: 1433: 1428: 1424: 1420: 1416: 1412: 1411: 1406: 1399: 1397: 1393: 1382: 1378: 1372: 1369: 1364: 1360: 1354: 1351: 1347: 1344:See the NASA 1341: 1338: 1323: 1317: 1314: 1309: 1305: 1298: 1291: 1289: 1287: 1285: 1281: 1275: 1271: 1264: 1261: 1255: 1252: 1243: 1236: 1228: 1225: 1217: 1210: 1208: 1206: 1204: 1200: 1196: 1192: 1189: 1183: 1181: 1177: 1173: 1167: 1164: 1159: 1155: 1151: 1147: 1142: 1137: 1133: 1129: 1125: 1121: 1117: 1110: 1107: 1102: 1098: 1094: 1090: 1083: 1080: 1077: 1071: 1068: 1063: 1059: 1055: 1051: 1044: 1042: 1040: 1036: 1031: 1024: 1021:York (1971). 1017: 1014: 1008: 1004: 1000: 992: 985: 977: 973: 969: 961: 958: 953: 946: 940: 937: 931: 927: 924: 922: 919: 918: 914: 912: 910: 908: 903: 899: 898: 893: 891: 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283: 279: 274: 272: 268: 267:least-squares 264: 260: 256: 255:-body problem 254: 249: 245: 241: 237: 233: 229: 221: 219: 217: 213: 209: 205: 204: 198: 196: 192: 188: 184: 180: 176: 172: 168: 164: 160: 157:in May 1980, 156: 152: 148: 143: 138: 136: 132: 128: 124: 120: 116: 113:mainframe in 112: 108: 103: 101: 100:magnetic tape 97: 93: 89: 81: 79: 77: 73: 69: 65: 61: 58: 54: 53:accelerations 50: 46: 42: 38: 34: 30: 26: 22: 19:(abbreviated 18: 2142: 2120: 2081:JPL FTP site 2023: 2009: 1992: 1980:. Retrieved 1970: 1962:the original 1952: 1943: 1933: 1919: 1911:the original 1907:"README.txt" 1888:"README.txt" 1881: 1872: 1859: 1851:the original 1840: 1831: 1818: 1809: 1796: 1787: 1774: 1730: 1726: 1715: 1705: 1679: 1666: 1657: 1644: 1618: 1614: 1600: 1588:. Retrieved 1581:the original 1567: 1556:the original 1551: 1538: 1521: 1517: 1511: 1503:the original 1492: 1481:the original 1476: 1463: 1449: 1414: 1408: 1384:. Retrieved 1380: 1371: 1362: 1353: 1340: 1328:. 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The 111:Univac 88:JPL DE 29:models 21:JPL DE 2147:(PDF) 2001:(PDF) 1869:(PDF) 1828:(PDF) 1806:(PDF) 1784:(PDF) 1761:S2CID 1735:arXiv 1702:(PDF) 1676:(PDF) 1654:(PDF) 1584:(PDF) 1577:(PDF) 1559:(PDF) 1548:(PDF) 1484:(PDF) 1473:(PDF) 1346:SPICE 1325:(PDF) 1245:(PDF) 1238:(PDF) 1219:(PDF) 1154:S2CID 1026:(PDF) 987:(PDF) 948:(PDF) 885:DE438 873:DE436 867:DE432 860:DE431 849:DE430 839:DE424 829:DE423 817:DE422 806:DE421 780:DE418 734:DE414 716:Pluto 712:DE413 706:DE412 700:DE411 679:DE410 639:DE409 633:DE408 627:DE407 620:DE406 603:DE405 588:DE404 561:DE403 555:DE402 549:DE202 537:DE200 531:DE102 519:DE441 507:DE440 466:DE430 458:DE405 450:DE200 419:DE406 395:DE405 329:DE102 226:Each 216:DE430 212:DE405 208:DE200 195:DE441 191:DE440 175:DE118 171:DE200 167:DE102 163:DE200 159:DE118 155:DE111 151:DE102 127:DE405 119:DE102 107:DE405 72:Pluto 2126:ISBN 1984:2016 1604:See 1437:ISSN 1332:2022 1294:See 1231:See 1146:ISSN 907:Juno 900:and 878:Juno 774:Eros 756:and 690:and 671:and 442:The 407:Mars 353:and 315:and 309:VLBI 265:. A 193:and 147:DE96 96:DE19 92:DE69 76:Moon 70:and 51:and 1944:JPL 1753:doi 1731:720 1631:doi 1619:187 1522:172 1427:doi 1415:161 1136:doi 1124:161 1093:233 1054:125 952:JPL 728:CCD 688:MER 684:IAU 383:FTP 367:eph 363:TDB 359:IAU 338:eph 323:of 317:CCD 133:in 64:Sun 39:in 2160:: 1942:. 1897:^ 1871:. 1830:. 1808:. 1786:. 1759:. 1751:. 1743:. 1729:. 1725:. 1704:. 1688:^ 1678:. 1656:. 1629:. 1617:. 1550:. 1520:. 1475:. 1435:. 1425:. 1413:. 1407:. 1395:^ 1379:. 1361:. 1283:^ 1202:^ 1179:^ 1152:. 1144:. 1134:. 1122:. 1118:. 1091:. 1052:. 1038:^ 1028:. 1001:. 995:; 989:. 980:; 970:. 950:. 911:. 655:, 390:. 300:. 137:. 125:. 102:. 47:, 25:DE 2135:. 2031:. 2017:. 1986:. 1946:. 1890:. 1875:. 1834:. 1812:. 1790:. 1767:. 1755:: 1747:: 1737:: 1708:. 1682:. 1660:. 1637:. 1633:: 1625:: 1609:. 1593:. 1532:. 1528:: 1457:. 1443:. 1429:: 1421:: 1389:. 1365:. 1334:. 1221:. 1174:. 1160:. 1138:: 1130:: 1103:. 1099:: 1064:. 1060:: 1032:. 1009:. 1005:: 993:. 954:. 909:) 486:. 475:. 468:. 439:. 336:T 253:n

Index

models
Solar System
Jet Propulsion Laboratory
Pasadena, California
positions
velocities
accelerations
Barycentric
rectangular coordinates
Sun
planets
Pluto
Moon
magnetic tape
Univac
double precision
Univac 1100/81
DEC Alpha
quadruple precision
theoretical work of the 1890s
J2000.0 reference frame
fundamental ephemeris
International Celestial Reference Frame
Astronomical Almanac
ephemeris
numerical integration
equations of motion
analytical
general perturbations
special perturbations

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