SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 HN2

2014 HN2

2014 HN2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.927 AU and a period of 0.89 yr.

Aten Observations: 66
Orbital Period · P
0.89 yr
v(q)
34.8 km/s
v(Q)
27.5 km/s
Diameter · ≈
0.02 km
TJ
6.45
Eccentricity · e
0.1179

Orbit and dynamics

The path is an ellipse reaching 0.818 AU from the Sun at perihelion and 1.036 AU at aphelion, a radial span of 0.218 AU.

Applying Kepler's third law to a = 0.927 AU gives an orbital period of 0.89 yr, or about 326 days.

An eccentricity of 0.118 makes the orbit moderately elongated.

Its inclination of 1.24° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.8 km/s at perihelion and falls to 27.5 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 = 26.34 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 66 observations and has a weighted RMS residual of 0.3792 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
0.9271 AU
Eccentricity
0.1179
Perihelion
0.818 AU
Aphelion
1.036405 AU
Inclination
1.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
16.38°

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
2030-Mar-25 07:52 0.322238 AU
48206110 km
12.84 km/s
2030-Nov-15 19:54 0.170026 AU
25435557 km
4.74 km/s
2031-Jun-13 11:08 0.186708 AU
27931165 km
8.63 km/s
2039-Jan-10 08:41 0.119639 AU
17897752 km
2.77 km/s
2039-Jun-12 11:47 0.019300 AU
2887197 km
3.08 km/s
2046-Apr-02 12:37 0.440853 AU
65950653 km
16.82 km/s
2046-Dec-14 21:21 0.151938 AU
22729563 km
4.15 km/s
2047-Jun-15 12:20 0.080725 AU
12076355 km
5.90 km/s
2054-Mar-27 22:08 0.280519 AU
41965093 km
12.80 km/s
2055-Jun-11 18:42 0.189810 AU
28395244 km
10.00 km/s
2062-Mar-21 20:47 0.110343 AU
16507013 km
8.17 km/s
2063-Jun-06 06:44 0.324726 AU
48578364 km
14.48 km/s
2070-Mar-19 08:43 0.004174 AU
624422 km
4.04 km/s
2078-Mar-18 22:15 0.006982 AU
1044485 km
5.44 km/s
2079-Jun-06 00:23 0.217442 AU
32528908 km
16.13 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
26.34

Orbit Quality

RMS
0.37921
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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