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Planetary Orbital Elements
Planetary Mean Orbits (J2000)
(epoch = J2000 = 2000 January 1.5)
(see the table of rates below) |
Planet (mean) | a AU | e |
i deg | Ω deg | ϖ deg | L deg |
|
Mercury | 0.38709893 | 0.20563069 |
7.00487 | 48.33167 | 77.45645 | 252.25084 |
Venus | 0.72333199 | 0.00677323 |
3.39471 | 76.68069 | 131.53298 | 181.97973 |
Earth | 1.00000011 | 0.01671022 |
0.00005 | -11.26064 | 102.94719 | 100.46435 |
Mars | 1.52366231 | 0.09341233 |
1.85061 | 49.57854 | 336.04084 | 355.45332 |
Jupiter | 5.20336301 | 0.04839266 |
1.30530 | 100.55615 | 14.75385 | 34.40438 |
Saturn | 9.53707032 | 0.05415060 |
2.48446 | 113.71504 | 92.43194 | 49.94432 |
Uranus | 19.19126393 | 0.04716771 |
0.76986 | 74.22988 | 170.96424 | 313.23218 |
Neptune | 30.06896348 | 0.00858587 |
1.76917 | 131.72169 | 44.97135 | 304.88003 |
Pluto | 39.48168677 | 0.24880766 |
17.14175 | 110.30347 | 224.06676 | 238.92881 |
|
|
Planetary Orbital Element Centennial Rates
(for the mean elements given above) |
Planet (rate) | a AU/Cy | e /Cy |
i "/Cy | Ω "/Cy | ϖ "/Cy |
L "/Cy |
|
Mercury | 0.00000066 | 0.00002527 |
-23.51 | -446.30 | 573.57 | 538101628.29 |
Venus | 0.00000092 | -0.00004938 |
-2.86 | -996.89 | -108.80 | 210664136.06 |
Earth | -0.00000005 | -0.00003804 |
-46.94 | -18228.25 | 1198.28 | 129597740.63 |
Mars | -0.00007221 | 0.00011902 |
-25.47 | -1020.19 | 1560.78 | 68905103.78 |
Jupiter | 0.00060737 | -0.00012880 |
-4.15 | 1217.17 | 839.93 | 10925078.35 |
Saturn | -0.00301530 | -0.00036762 |
6.11 | -1591.05 | -1948.89 | 4401052.95 |
Uranus | 0.00152025 | -0.00019150 |
-2.09 | -1681.40 | 1312.56 | 1542547.79 |
Neptune | -0.00125196 | 0.0000251 |
-3.64 | -151.25 | -844.43 | 786449.21 |
Pluto | -0.00076912 | 0.00006465 |
11.07 | -37.33 | -132.25 | 522747.90 |
|
|
Legend:
" arcseconds
Cy Julian century
a semi-major axis
e eccentricity
i inclination
Ω longitude of the ascending node
ϖ longitude of perihelion
L mean longitude
Notes:
This table contains mean orbit solutions from a 250 yr. least squares fit
of the DE 200 planetary ephemeris to a Keplerian orbit where each element
is allowed to vary linearly with time.
This solution fits the terrestrial planet orbits to ~25" or better,
but achieves only ~600" for Saturn.
Elements are referenced to mean ecliptic and equinox of J2000
at the J2000 epoch (2451545.0 JD).
Reference:
Explanatory Supplement to the Astronomical Almanac. 1992.
K. P. Seidelmann, Ed., p.316 (Table 5.8.1),
University Science Books, Mill Valley, California.