Orbit and dynamics
The path is an ellipse reaching 1.01 AU from the Sun at perihelion and 1.924 AU at aphelion, a radial span of 0.914 AU.
Applying Kepler's third law to a = 1.467 AU gives an orbital period of 1.78 yr, or about 649 days.
An eccentricity of 0.311 makes the orbit moderately elongated.
A steep inclination of 35.54° carries it well above and below the ecliptic plane.
By the vis-viva equation its orbital speed rises to 33.9 km/s at perihelion and falls to 17.8 km/s at aphelion.
Size and surface
No direct size measurement is available; from an absolute magnitude of H = 21.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.
Observation record and orbit quality
The current orbit solution is based on 69 observations and has a weighted RMS residual of 0.6222 arcseconds.
Condition code U = 2 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 |
|---|---|---|
| 2032-Jan-31 15:31 | 0.189301 AU 28318976 km |
19.64 km/s |
| 2048-Jan-29 00:14 | 0.120539 AU 18032382 km |
19.57 km/s |
| 2064-Jan-27 09:23 | 0.080773 AU 12083534 km |
19.64 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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