SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 XU6

2014 XU6

2014 XU6 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.76 AU and a period of 0.66 yr.

Aten Observations: 68
Orbital Period · P
0.66 yr
v(q)
54.4 km/s
v(Q)
21.5 km/s
Diameter · ≈
0.06 km
TJ
7.44
Eccentricity · e
0.4343

Orbit and dynamics

Between its closest point (0.43 AU) and its farthest (1.09 AU), the heliocentric distance changes by 0.66 AU over every revolution.

One full revolution takes 0.66 yr (242 days), computed from the semi-major axis of 0.76 AU.

The high eccentricity (0.434) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 30.73° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 54.4 km/s at perihelion and falls to 21.5 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 = 24 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 68 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4733 arcseconds.

Condition code U = 1 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
0.7601 AU
Eccentricity
0.4343
Perihelion
0.43 AU
Aphelion
1.090211 AU
Inclination
30.73°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
316.31°

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
2026-Dec-19 09:52 0.268564 AU
40176676 km
20.72 km/s
2028-Dec-18 06:25 0.323607 AU
48410902 km
22.36 km/s
2030-Dec-17 14:46 0.381818 AU
57119234 km
24.18 km/s
2032-Dec-15 13:16 0.442123 AU
66140692 km
26.11 km/s
2051-Nov-26 14:19 0.459749 AU
68777466 km
23.74 km/s
2053-Nov-25 17:08 0.408665 AU
61135475 km
21.98 km/s
2055-Nov-26 10:55 0.359953 AU
53848148 km
20.43 km/s
2057-Nov-26 21:04 0.313931 AU
46963425 km
19.09 km/s
2059-Nov-28 22:58 0.271117 AU
40558514 km
18.02 km/s
2061-Nov-30 13:26 0.231613 AU
34648878 km
17.22 km/s
2063-Dec-03 11:56 0.195035 AU
29176837 km
16.67 km/s
2065-Dec-05 15:52 0.161037 AU
24090817 km
16.31 km/s
2067-Dec-08 21:30 0.130829 AU
19571713 km
16.13 km/s
2069-Dec-11 00:44 0.107229 AU
16041261 km
16.10 km/s
2071-Dec-13 23:12 0.095390 AU
14270204 km
16.23 km/s
2073-Dec-15 15:10 0.100842 AU
15085752 km
16.54 km/s
2075-Dec-17 22:04 0.124312 AU
18596858 km
17.09 km/s
2077-Dec-18 17:14 0.160574 AU
24021598 km
17.91 km/s
2079-Dec-19 22:19 0.205320 AU
30715421 km
19.01 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
24.0

Orbit Quality

RMS
0.47334
Condition
1
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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