SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 HZ2

2026 HZ2

2026 HZ2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.132 AU it takes 1.20 yr to circle the Sun.

Apollo Observations: 54
Orbital Period · P
1.20 yr
v(q)
37.6 km/s
v(Q)
20.8 km/s
TJ
5.49
Eccentricity · e
0.2869

Orbit and dynamics

Between its closest point (0.807 AU) and its farthest (1.457 AU), the heliocentric distance changes by 0.65 AU over every revolution.

One full revolution takes 1.20 yr (440 days), computed from the semi-major axis of 1.132 AU.

An eccentricity of 0.287 makes the orbit moderately elongated.

Its inclination of 4.3° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.6 km/s at perihelion and falls to 20.8 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2026 HZ2, so its physical size remains unconstrained.

Observation record and orbit quality

Astrometry from 54 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3406 arcseconds.

Condition code U = 5 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
1.132 AU
Eccentricity
0.2869
Perihelion
0.807 AU
Aphelion
1.456771 AU
Inclination
4.3°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
345.92°

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
2032-May-07 15:22 0.109391 AU
16364588 km
6.07 km/s
2038-Jun-17 19:53 0.192390 AU
28781090 km
7.52 km/s
2050-Aug-18 21:47 0.189826 AU
28397558 km
7.44 km/s
2056-Sep-30 23:24 0.082822 AU
12390027 km
6.02 km/s
2062-Oct-13 22:18 0.017592 AU
2631745 km
9.51 km/s
2073-Apr-19 06:01 0.007289 AU
1090491 km
11.51 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
30.49

Orbit Quality

RMS
0.34064
Condition
5
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.