Orbit and dynamics
The path is an ellipse reaching 0.958 AU from the Sun at perihelion and 2.442 AU at aphelion, a radial span of 1.484 AU.
Applying Kepler's third law to a = 1.7 AU gives an orbital period of 2.22 yr, or about 810 days.
The high eccentricity (0.436) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.
Its inclination of 3° keeps it close to the plane of the ecliptic.
By the vis-viva equation its orbital speed rises to 36.5 km/s at perihelion and falls to 14.3 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
Neither a measured diameter nor a reliable absolute magnitude is available for 2023 VD2, so its physical size remains unconstrained.
Observation record and orbit quality
The current orbit solution is based on 24 observations and has a weighted RMS residual of 0.5029 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 |
|---|---|---|
| 2035-Feb-01 08:14 | 0.305606 AU 45717974 km |
18.26 km/s |
| 2043-Oct-07 20:07 | 0.165789 AU 24801718 km |
15.52 km/s |
| 2074-Dec-08 05:02 | 0.036389 AU 5443650 km |
6.48 km/s |
Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.
Physical Parameters
Orbit Quality
Related Objects
Same object type
Similar orbit
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