Orbit and dynamics
The path is an ellipse reaching 0.68 AU from the Sun at perihelion and 1.283 AU at aphelion, a radial span of 0.603 AU.
Applying Kepler's third law to a = 0.981 AU gives an orbital period of 0.97 yr, or about 355 days.
An eccentricity of 0.307 makes the orbit moderately elongated.
A steep inclination of 21.45° carries it well above and below the ecliptic plane.
By the vis-viva equation its orbital speed rises to 41.3 km/s at perihelion and falls to 21.9 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
No direct size measurement is available; from an absolute magnitude of H = 26.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.
Observation record and orbit quality
The current orbit solution is based on 17 observations and has a weighted RMS residual of 0.6389 arcseconds.
Condition code U = 8 signals a poorly constrained orbit, so its future path should be treated as provisional.
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 |
|---|---|---|
| 2062-Jan-29 12:03 | 0.202218 AU 30251413 km |
18.82 km/s |
| 2063-Jan-18 13:41 | 0.362021 AU 54157500 km |
23.08 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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