Orbit and dynamics
The path is an ellipse reaching 0.745 AU from the Sun at perihelion and 1.801 AU at aphelion, a radial span of 1.056 AU.
Applying Kepler's third law to a = 1.273 AU gives an orbital period of 1.44 yr, or about 525 days.
The high eccentricity (0.414) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.
The orbital plane is tilted 16.08° relative to the ecliptic.
By the vis-viva equation its orbital speed rises to 41 km/s at perihelion and falls to 17 km/s at aphelion.
Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.
Size and surface
The measured diameter is 0.32 km, a value from direct size determination rather than from brightness alone.
Observation record and orbit quality
The current orbit solution is based on 586 observations and has a weighted RMS residual of 0.4734 arcseconds.
Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.
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-Apr-07 04:32 | 0.032233 AU 4821914 km |
13.46 km/s |
| 2044-Oct-22 20:59 | 0.065063 AU 9733344 km |
13.72 km/s |
| 2052-Apr-16 17:22 | 0.152269 AU 22779130 km |
18.05 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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