Orbit and dynamics
The path is an ellipse reaching 1.002 AU from the Sun at perihelion and 2.63 AU at aphelion, a radial span of 1.628 AU.
Applying Kepler's third law to a = 1.816 AU gives an orbital period of 2.45 yr, or about 894 days.
The high eccentricity (0.448) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.
The orbital plane is tilted 6.21° relative to the ecliptic.
By the vis-viva equation its orbital speed rises to 35.8 km/s at perihelion and falls to 13.6 km/s at aphelion.
Size and surface
No direct size measurement is available; from an absolute magnitude of H = 25.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.
Observation record and orbit quality
The current orbit solution is based on 105 observations and has a weighted RMS residual of 0.3709 arcseconds.
Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.
About these computed values
Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.
Orbital Parameters
Orbit diagram
The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.
3D orbit (interactive)
Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.
Close approaches
Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).
| Date (UTC) | Miss distance | Velocity |
|---|---|---|
| 2042-Jan-30 06:28 | 0.273044 AU 40846760 km |
19.34 km/s |
| 2059-May-21 07:42 | 0.241034 AU 36058152 km |
17.38 km/s |
Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.
Physical Parameters
Orbit Quality
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