SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 HG4

2014 HG4

2014 HG4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.766 AU it takes 4.60 yr to circle the Sun.

Apollo Observations: 194
Orbital Period · P
4.60 yr
v(q)
52 km/s
v(Q)
6.2 km/s
Diameter · ≈
0.36 km
TJ
2.78
Eccentricity · e
0.7879

Orbit and dynamics

The path is an ellipse reaching 0.587 AU from the Sun at perihelion and 4.945 AU at aphelion, a radial span of 4.358 AU.

Applying Kepler's third law to a = 2.766 AU gives an orbital period of 4.60 yr, or about 1,680 days.

The high eccentricity (0.788) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.54° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 52 km/s at perihelion and falls to 6.2 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 0.97 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.022 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 194 observations and has a weighted RMS residual of 0.3961 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
2.766 AU
Eccentricity
0.7879
Perihelion
0.587 AU
Aphelion
4.945331 AU
Inclination
4.54°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
210.75°

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
2037-May-14 19:51 0.071728 AU
10730424 km
22.78 km/s
2046-Nov-13 07:58 0.120977 AU
18097876 km
26.00 km/s
2060-Aug-27 07:25 0.409179 AU
61212376 km
21.67 km/s
2079-Oct-14 15:55 0.214166 AU
32038755 km
16.09 km/s

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

Physical Parameters

Diameter
0.975 km
Albedo
0.022
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.95

Orbit Quality

RMS
0.3961
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.