SpaceAtlas Space Object Data
NASA JPL SBDB · 2002 UQ12

2002 UQ12

2002 UQ12 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.76 AU it takes 2.33 yr to circle the Sun.

Apollo Observations: 153
Orbital Period · P
2.33 yr
v(q)
53.3 km/s
v(Q)
9.5 km/s
Diameter · ≈
0.12 km
TJ
3.79
Eccentricity · e
0.6986

Orbit and dynamics

The path is an ellipse reaching 0.531 AU from the Sun at perihelion and 2.99 AU at aphelion, a radial span of 2.459 AU.

Applying Kepler's third law to a = 1.76 AU gives an orbital period of 2.33 yr, or about 853 days.

The high eccentricity (0.699) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.86° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 53.3 km/s at perihelion and falls to 9.5 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 = 22.39 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 153 observations and has a weighted RMS residual of 0.5389 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
1.76 AU
Eccentricity
0.6986
Perihelion
0.531 AU
Aphelion
2.989536 AU
Inclination
2.86°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
16.97°

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
2030-Nov-13 17:03 0.141863 AU
21222438 km
17.19 km/s
2037-Nov-18 12:35 0.205551 AU
30750008 km
15.27 km/s
2044-Nov-28 19:15 0.279454 AU
41805677 km
13.58 km/s
2051-Dec-19 15:22 0.351646 AU
52605441 km
15.72 km/s
2059-Jan-03 19:04 0.398388 AU
59597964 km
18.71 km/s
2066-Jan-17 15:10 0.431384 AU
64534075 km
21.17 km/s
2073-Jan-31 03:18 0.448572 AU
67105371 km
22.59 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
22.39

Orbit Quality

RMS
0.53888
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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