SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 HM4

2014 HM4

2014 HM4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.099 AU it takes 1.15 yr to circle the Sun.

Apollo Observations: 34
Orbital Period · P
1.15 yr
v(q)
51.2 km/s
v(Q)
15.7 km/s
Diameter · ≈
0.01 km
TJ
5.51
Eccentricity · e
0.53

Orbit and dynamics

The path is an ellipse reaching 0.517 AU from the Sun at perihelion and 1.681 AU at aphelion, a radial span of 1.164 AU.

Applying Kepler's third law to a = 1.099 AU gives an orbital period of 1.15 yr, or about 421 days.

The high eccentricity (0.53) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 1.31° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 51.2 km/s at perihelion and falls to 15.7 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 = 26.9 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 34 observations and has a weighted RMS residual of 0.5111 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
1.099 AU
Eccentricity
0.53
Perihelion
0.517 AU
Aphelion
1.68147 AU
Inclination
1.31°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
137.07°

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
2029-Apr-19 16:59 0.137600 AU
20584634 km
21.20 km/s
2030-Aug-02 11:49 0.487005 AU
72854854 km
20.89 km/s
2031-Dec-08 08:47 0.209536 AU
31346197 km
11.00 km/s
2037-Apr-29 05:31 0.251161 AU
37573183 km
10.22 km/s
2038-Sep-10 18:11 0.479311 AU
71703876 km
20.71 km/s
2039-Dec-21 07:42 0.193336 AU
28922721 km
23.12 km/s
2044-Apr-14 01:19 0.259531 AU
38825299 km
25.12 km/s
2045-Jul-20 01:47 0.467293 AU
69905967 km
19.24 km/s
2046-Nov-02 23:35 0.335243 AU
50151683 km
10.56 km/s
2046-Dec-18 07:28 0.325084 AU
48631859 km
10.11 km/s
2052-Apr-29 11:24 0.122362 AU
18305038 km
13.25 km/s
2053-Aug-29 05:51 0.491544 AU
73533974 km
21.64 km/s
2054-Dec-15 23:46 0.069938 AU
10462543 km
19.29 km/s
2059-Apr-10 17:57 0.358009 AU
53557393 km
28.13 km/s
2060-Apr-01 07:42 0.487402 AU
72914236 km
11.81 km/s
2060-Jul-09 15:28 0.445611 AU
66662494 km
17.48 km/s
2061-Oct-17 20:09 0.388746 AU
58155545 km
14.04 km/s
2061-Dec-26 05:05 0.396555 AU
59323771 km
10.81 km/s
2067-Apr-29 10:19 0.092831 AU
13887391 km
14.22 km/s
2068-Aug-26 17:22 0.492897 AU
73736386 km
21.70 km/s
2069-Dec-15 05:04 0.057971 AU
8672338 km
18.88 km/s
2074-Apr-11 14:31 0.331723 AU
49625092 km
27.38 km/s
2075-Jul-14 13:39 0.454016 AU
67919882 km
18.20 km/s
2076-Oct-25 12:42 0.359407 AU
53766501 km
12.29 km/s
2076-Dec-21 12:55 0.355631 AU
53201595 km
10.40 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
26.9

Orbit Quality

RMS
0.51105
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.

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