SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 UU3

2005 UU3

2005 UU3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.282 AU it takes 1.45 yr to circle the Sun.

Apollo Observations: 60
Orbital Period · P
1.45 yr
v(q)
44.2 km/s
v(Q)
15.6 km/s
Diameter · ≈
0.13 km
TJ
4.91
Eccentricity · e
0.4779

Orbit and dynamics

The path is an ellipse reaching 0.67 AU from the Sun at perihelion and 1.895 AU at aphelion, a radial span of 1.225 AU.

Applying Kepler's third law to a = 1.282 AU gives an orbital period of 1.45 yr, or about 530 days.

The high eccentricity (0.478) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.94° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.2 km/s at perihelion and falls to 15.6 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 = 22.17 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

The current orbit solution is based on 60 observations and has a weighted RMS residual of 0.7254 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
1.282 AU
Eccentricity
0.4779
Perihelion
0.67 AU
Aphelion
1.894668 AU
Inclination
13.94°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
3.69°

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
2029-Jun-19 15:23 0.333971 AU
49961391 km
23.53 km/s
2032-Apr-22 15:12 0.263150 AU
39366718 km
13.67 km/s
2034-Nov-27 19:22 0.339972 AU
50859125 km
9.80 km/s
2035-Jan-24 16:04 0.334552 AU
50048256 km
11.34 km/s
2037-Nov-20 08:44 0.324227 AU
48503600 km
23.64 km/s
2045-Jun-08 20:48 0.192119 AU
28740599 km
18.59 km/s
2048-Mar-28 17:42 0.326292 AU
48812600 km
15.14 km/s
2050-Dec-05 18:17 0.213870 AU
31994423 km
11.26 km/s
2053-Nov-14 23:56 0.444066 AU
66431281 km
27.50 km/s
2061-Jun-04 02:59 0.158083 AU
23648901 km
16.86 km/s
2064-Mar-27 08:55 0.329009 AU
49219066 km
15.23 km/s
2066-Dec-04 05:21 0.281140 AU
42057881 km
9.91 km/s
2069-Nov-22 23:50 0.283952 AU
42478542 km
22.28 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
22.17

Orbit Quality

RMS
0.72538
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.

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