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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.
Orbital Elements at Epoch 2454049.5 (2006-Nov-10.0) TDB
Reference: JPL 35 (heliocentric ecliptic J2000)
| Element | Value | Uncertainty (1-sigma) | Units |
| e | 1.000185049039808 | 1.7109e-06 | |
| a | -4231.355298769043 | 39.12 | au |
| q | .7830082351241019 | 3.5988e-07 | au |
| i | 111.8232624168263 | 2.9769e-05 | deg |
| node | 148.7268421584153 | 2.8409e-05 | deg |
| peri | 62.59437100123628 | 5.6879e-05 | deg |
| M | .0001513674291051965 | 2.099e-06 | deg |
| tp | 2454007.228505602883
(2006-Sep-28.72850560) | 3.8294e-05 | TDB |
| period | n/a
n/a | n/a
n/a | d
yr |
| n | 3.5808393165187E-6 | 4.9658e-08 | deg/d |
| Q | n/a | n/a | au |
|
| | Orbit Determination Parameters
Additional Information
|
[ hide covariance matrix ]
Orbit Covariance (6×6)
|
| |
e |
q |
tp |
node |
peri |
i |
| e |
2.927017162243796E-12 |
3.264409369631496E-13 |
5.697927284624324E-11 |
-6.670812516900478E-12 |
7.487755190346444E-11 |
-1.785926927231847E-11 |
| q |
3.264409369631496E-13 |
1.29515682692476E-13 |
8.51191863710928E-12 |
4.878328376341891E-13 |
1.678668708421835E-11 |
-4.493320608310402E-12 |
| tp |
5.697927284624324E-11 |
8.51191863710928E-12 |
1.466420751894591E-9 |
-2.590838039784736E-11 |
1.987561437665246E-9 |
-3.017002841440008E-10 |
| node |
-6.670812516900478E-12 |
4.878328376341891E-13 |
-2.590838039784736E-11 |
8.070888174770137E-10 |
2.642422847865895E-10 |
-4.145628339379156E-10 |
| peri |
7.487755190346444E-11 |
1.678668708421835E-11 |
1.987561437665246E-9 |
2.642422847865895E-10 |
3.235191315690719E-9 |
-6.881936060822833E-10 |
| i |
-1.785926927231847E-11 |
-4.493320608310402E-12 |
-3.017002841440008E-10 |
-4.145628339379156E-10 |
-6.881936060822833E-10 |
8.861690290414364E-10 |
|
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