SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 RL12

2014 RL12

2014 RL12 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.761 AU it takes 4.59 yr to circle the Sun.

Apollo Observations: 325
Orbital Period · P
4.59 yr
v(q)
40.6 km/s
v(Q)
7.9 km/s
Diameter · ≈
0.91 km
TJ
2.87
Eccentricity · e
0.6735

Orbit and dynamics

Between its closest point (0.902 AU) and its farthest (4.621 AU), the heliocentric distance changes by 3.719 AU over every revolution.

One full revolution takes 4.59 yr (1,676 days), computed from the semi-major axis of 2.761 AU.

The high eccentricity (0.673) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 23.79° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.6 km/s at perihelion and falls to 7.9 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 0.69 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.254 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 325 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3442 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
2.761 AU
Eccentricity
0.6735
Perihelion
0.902 AU
Aphelion
4.620534 AU
Inclination
23.79°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
189.21°

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
2037-Dec-04 05:53 0.266965 AU
39937368 km
14.39 km/s
2060-Dec-05 04:32 0.244765 AU
36616317 km
14.82 km/s

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

Physical Parameters

Diameter
0.694 km
Albedo
0.254
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
17.96

Orbit Quality

RMS
0.34421
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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