SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 HH4

2026 HH4

2026 HH4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.88 AU and a period of 0.83 yr.

Aten Observations: 52
Orbital Period · P
0.83 yr
v(q)
57.2 km/s
v(Q)
17.6 km/s
Diameter · ≈
0.01 km
TJ
6.61
Eccentricity · e
0.5289

Orbit and dynamics

Between its closest point (0.415 AU) and its farthest (1.345 AU), the heliocentric distance changes by 0.93 AU over every revolution.

One full revolution takes 0.83 yr (301 days), computed from the semi-major axis of 0.88 AU.

The high eccentricity (0.529) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 0.33° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 57.2 km/s at perihelion and falls to 17.6 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 = 27.14 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 52 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4852 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
0.8798 AU
Eccentricity
0.5289
Perihelion
0.415 AU
Aphelion
1.345126 AU
Inclination
0.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
131.77°

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-Jul-18 09:06 0.193662 AU
28971381 km
10.90 km/s
2032-Jul-25 04:26 0.036110 AU
5401972 km
16.72 km/s
2040-Apr-27 03:25 0.112809 AU
16876032 km
19.26 km/s
2045-Apr-26 06:35 0.113166 AU
16929361 km
11.47 km/s
2046-Jul-27 03:36 0.037627 AU
5628975 km
13.01 km/s
2059-Apr-24 10:04 0.005506 AU
823632 km
15.50 km/s
2064-May-02 07:44 0.180337 AU
26978088 km
10.90 km/s
2065-Jul-27 04:06 0.002710 AU
405342 km
14.67 km/s
2070-Jul-22 14:25 0.070746 AU
10583396 km
20.03 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
27.14

Orbit Quality

RMS
0.48523
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.