SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 AE29

2014 AE29

2014 AE29 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.907 AU and a period of 0.86 yr.

Aten Observations: 26
Orbital Period · P
0.86 yr
v(q)
36.7 km/s
v(Q)
26.7 km/s
Diameter · ≈
0.01 km
TJ
6.56
Eccentricity · e
0.1579

Orbit and dynamics

The path is an ellipse reaching 0.764 AU from the Sun at perihelion and 1.051 AU at aphelion, a radial span of 0.287 AU.

Applying Kepler's third law to a = 0.907 AU gives an orbital period of 0.86 yr, or about 316 days.

An eccentricity of 0.158 makes the orbit moderately elongated.

Its inclination of 4.86° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.7 km/s at perihelion and falls to 26.7 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

No direct size measurement is available; from an absolute magnitude of H = 27.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 26 observations and has a weighted RMS residual of 0.2799 arcseconds.

Condition code U = 6 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
0.9074 AU
Eccentricity
0.1579
Perihelion
0.764 AU
Aphelion
1.050678 AU
Inclination
4.86°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
12.67°

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-Jan-10 03:39 0.209493 AU
31339714 km
11.50 km/s
2032-Aug-08 23:54 0.172741 AU
25841695 km
4.70 km/s
2032-Dec-25 18:07 0.044725 AU
6690789 km
4.05 km/s
2038-Oct-08 02:57 0.128386 AU
19206332 km
7.66 km/s
2039-Apr-24 22:14 0.239579 AU
35840471 km
6.65 km/s
2039-Dec-31 20:48 0.471007 AU
70461638 km
19.49 km/s
2044-Oct-19 00:14 0.447200 AU
66900214 km
18.09 km/s
2045-Jun-25 07:38 0.235945 AU
35296823 km
7.13 km/s
2046-Jan-12 06:19 0.136576 AU
20431433 km
8.89 km/s
2051-Nov-02 13:00 0.089051 AU
13321779 km
3.83 km/s
2052-Mar-17 15:41 0.191652 AU
28670673 km
4.20 km/s
2057-Oct-13 09:13 0.280519 AU
41965098 km
13.20 km/s
2058-May-27 19:43 0.251189 AU
37577286 km
7.55 km/s
2059-Jan-07 12:11 0.279354 AU
41790808 km
13.89 km/s
2064-Jul-28 01:37 0.188252 AU
28162154 km
5.49 km/s
2065-Jan-06 12:28 0.011884 AU
1777785 km
4.55 km/s
2070-Oct-08 19:06 0.183815 AU
27498359 km
9.79 km/s
2071-May-08 18:07 0.245898 AU
36785863 km
7.18 km/s
2072-Jan-03 21:21 0.386172 AU
57770556 km
16.86 km/s
2077-Jul-27 18:40 0.191449 AU
28640334 km
5.43 km/s
2078-Jan-05 11:35 0.022396 AU
3350431 km
4.41 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
27.4

Orbit Quality

RMS
0.2799
Condition
6
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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