SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 OO6

2014 OO6

2014 OO6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.201 AU it takes 3.27 yr to circle the Sun.

Apollo Observations: 99
Orbital Period · P
3.27 yr
v(q)
45.9 km/s
v(Q)
8.8 km/s
Diameter · ≈
0.09 km
TJ
3.32
Eccentricity · e
0.6783

Orbit and dynamics

Between its closest point (0.708 AU) and its farthest (3.694 AU), the heliocentric distance changes by 2.986 AU over every revolution.

One full revolution takes 3.27 yr (1,193 days), computed from the semi-major axis of 2.201 AU.

The high eccentricity (0.678) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.38° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 45.9 km/s at perihelion and falls to 8.8 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 = 23.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

Astrometry from 99 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4197 arcseconds.

Condition code U = 4 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
2.201 AU
Eccentricity
0.6783
Perihelion
0.708 AU
Aphelion
3.693938 AU
Inclination
1.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
206.99°

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
2027-Oct-24 10:34 0.283577 AU
42422484 km
15.75 km/s
2040-Dec-05 13:33 0.229200 AU
34287849 km
14.02 km/s
2054-Jan-17 18:18 0.066839 AU
9998929 km
20.57 km/s
2063-Aug-07 00:39 0.147401 AU
22050857 km
22.37 km/s
2067-Feb-08 05:39 0.485405 AU
72615505 km
32.61 km/s
2076-Aug-19 14:50 0.026481 AU
3961488 km
16.64 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
23.1

Orbit Quality

RMS
0.41965
Condition
4
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.