SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 YU3

2005 YU3

2005 YU3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.553 AU it takes 4.08 yr to circle the Sun.

Apollo Observations: 82
Orbital Period · P
4.08 yr
v(q)
63.4 km/s
v(Q)
5.5 km/s
Diameter · ≈
0.39 km
TJ
2.8
Eccentricity · e
0.841

Orbit and dynamics

The path is an ellipse reaching 0.406 AU from the Sun at perihelion and 4.7 AU at aphelion, a radial span of 4.294 AU.

Applying Kepler's third law to a = 2.553 AU gives an orbital period of 4.08 yr, or about 1,490 days.

The high eccentricity (0.841) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.01° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 63.4 km/s at perihelion and falls to 5.5 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 = 19.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.39 km.

Observation record and orbit quality

The current orbit solution is based on 82 observations and has a weighted RMS residual of 0.5334 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

Semi-Major Axis
2.553 AU
Eccentricity
0.841
Perihelion
0.406 AU
Aphelion
4.700073 AU
Inclination
3.01°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
17.55°

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
2034-May-20 12:35 0.046029 AU
6885807 km
27.16 km/s
2042-Nov-16 21:30 0.380334 AU
56897103 km
17.45 km/s
2059-Apr-29 01:55 0.470682 AU
70412965 km
41.40 km/s
2063-Jul-13 11:00 0.461420 AU
69027401 km
20.77 km/s
2067-Oct-16 20:42 0.498985 AU
74647023 km
24.84 km/s
2072-Jan-10 03:54 0.449217 AU
67201858 km
41.00 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
19.8

Orbit Quality

RMS
0.53342
Condition
0
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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