SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 XK14

2004 XK14

2004 XK14 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.749 AU and a period of 0.65 yr.

Aten Observations: 152
Orbital Period · P
0.65 yr
v(q)
54.8 km/s
v(Q)
21.6 km/s
Diameter · ≈
0.12 km
TJ
7.64
Eccentricity · e
0.4339

Orbit and dynamics

Between its closest point (0.424 AU) and its farthest (1.073 AU), the heliocentric distance changes by 0.649 AU over every revolution.

One full revolution takes 0.65 yr (237 days), computed from the semi-major axis of 0.749 AU.

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

Its inclination of 3.1° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 54.8 km/s at perihelion and falls to 21.6 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 0.24 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.034 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 152 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4931 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
0.7485 AU
Eccentricity
0.4339
Perihelion
0.424 AU
Aphelion
1.073274 AU
Inclination
3.1°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
264.19°

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-Nov-19 03:49 0.087784 AU
13132235 km
8.72 km/s
2028-Aug-18 09:39 0.458387 AU
68573666 km
12.36 km/s
2029-Jan-01 02:52 0.062825 AU
9398513 km
12.28 km/s
2030-Dec-23 10:50 0.393432 AU
58856596 km
23.75 km/s
2035-Nov-07 02:23 0.234328 AU
35054965 km
18.05 km/s
2037-Nov-16 18:06 0.083234 AU
12451621 km
8.80 km/s
2039-Aug-20 09:33 0.454938 AU
68057728 km
12.05 km/s
2040-Jan-01 19:44 0.056587 AU
8465333 km
12.06 km/s
2041-Dec-23 06:47 0.392124 AU
58660914 km
23.71 km/s
2046-Nov-06 12:23 0.220063 AU
32920909 km
17.54 km/s
2048-Nov-20 05:48 0.089743 AU
13425367 km
8.69 km/s
2050-Aug-16 18:03 0.466298 AU
69757208 km
13.00 km/s
2051-Jan-01 17:28 0.079133 AU
11838135 km
12.88 km/s
2052-Dec-21 21:57 0.419862 AU
62810446 km
24.67 km/s
2057-Nov-05 08:39 0.185723 AU
27783768 km
16.31 km/s
2059-Nov-28 07:16 0.097200 AU
14540930 km
8.64 km/s
2061-Aug-11 01:45 0.483734 AU
72365593 km
14.49 km/s
2062-Jan-01 02:33 0.120604 AU
18042117 km
14.33 km/s
2063-Dec-20 20:25 0.465026 AU
69566838 km
26.25 km/s
2066-Nov-16 03:43 0.474724 AU
71017691 km
26.52 km/s
2068-Nov-04 03:35 0.140285 AU
20986334 km
14.66 km/s
2069-Mar-28 12:15 0.487179 AU
72880892 km
15.39 km/s
2070-Dec-07 12:20 0.096280 AU
14403308 km
8.63 km/s
2072-Dec-30 21:08 0.169037 AU
25287641 km
16.01 km/s
2077-Nov-14 00:28 0.427799 AU
63997881 km
24.85 km/s
2079-Nov-04 11:25 0.097742 AU
14621948 km
13.03 km/s

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

Physical Parameters

Diameter
0.24 km
Albedo
0.034
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
22.44

Orbit Quality

RMS
0.49313
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

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