SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 UD3

2024 UD3

2024 UD3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.868 AU it takes 2.55 yr to circle the Sun.

Apollo Observations: 29
Orbital Period · P
2.55 yr
v(q)
42.3 km/s
v(Q)
11.2 km/s
Diameter · ≈
0.07 km
TJ
3.76
Eccentricity · e
0.58

Orbit and dynamics

Between its closest point (0.784 AU) and its farthest (2.951 AU), the heliocentric distance changes by 2.167 AU over every revolution.

One full revolution takes 2.55 yr (933 days), computed from the semi-major axis of 1.868 AU.

The high eccentricity (0.58) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.85° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.3 km/s at perihelion and falls to 11.2 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 = 23.64 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

Astrometry from 29 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3338 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

Semi-Major Axis
1.868 AU
Eccentricity
0.58
Perihelion
0.784 AU
Aphelion
2.95144 AU
Inclination
4.85°
Orbital Period
— yr
Epoch
2460609.5
Mean Anomaly
339.4°

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 distanceVelocity
2065-Oct-06 04:07 0.361004 AU
54005374 km
27.22 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
23.64

Orbit Quality

RMS
0.33384
Condition
8
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. 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.

Keep exploring

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