SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 LU134

2010 LU134

2010 LU134 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.897 AU it takes 2.61 yr to circle the Sun.

Apollo Observations: 44
Orbital Period · P
2.61 yr
v(q)
39.9 km/s
v(Q)
11.7 km/s
Diameter · ≈
0.49 km
TJ
3.64
Eccentricity · e
0.5457

Orbit and dynamics

The path is an ellipse reaching 0.862 AU from the Sun at perihelion and 2.932 AU at aphelion, a radial span of 2.07 AU.

Applying Kepler's third law to a = 1.897 AU gives an orbital period of 2.61 yr, or about 954 days.

The high eccentricity (0.546) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 27.36° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.9 km/s at perihelion and falls to 11.7 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

The measured diameter is 0.32 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.443 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 44 observations and has a weighted RMS residual of 0.7751 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
1.897 AU
Eccentricity
0.5457
Perihelion
0.862 AU
Aphelion
2.932193 AU
Inclination
27.36°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
19.8°

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
2036-Oct-16 03:59 0.335543 AU
50196477 km
21.82 km/s
2044-Jul-11 12:00 0.489487 AU
73226184 km
24.10 km/s
2057-Aug-26 01:24 0.183750 AU
27488650 km
19.49 km/s
2070-Oct-11 11:55 0.294750 AU
44093953 km
21.08 km/s

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

Physical Parameters

Diameter
0.317 km
Albedo
0.443
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.31

Orbit Quality

RMS
0.77511
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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