SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 EU2

2026 EU2

2026 EU2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.069 AU it takes 1.11 yr to circle the Sun.

Apollo Observations: 77
Orbital Period · P
1.11 yr
v(q)
31.6 km/s
v(Q)
26.2 km/s
Diameter · ≈
0.01 km
TJ
5.75
Eccentricity · e
0.0933

Orbit and dynamics

Between its closest point (0.97 AU) and its farthest (1.169 AU), the heliocentric distance changes by 0.199 AU over every revolution.

One full revolution takes 1.11 yr (404 days), computed from the semi-major axis of 1.069 AU.

With e = 0.093, the orbit is close to circular.

The orbital plane is tilted 11.23° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.6 km/s at perihelion and falls to 26.2 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

No direct size measurement is available; from an absolute magnitude of H = 27.24 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 77 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3769 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
1.069 AU
Eccentricity
0.0933
Perihelion
0.97 AU
Aphelion
1.168738 AU
Inclination
11.23°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
39.74°

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
2047-Mar-17 10:33 0.031167 AU
4662569 km
6.12 km/s
2047-Sep-04 14:22 0.118544 AU
17733925 km
6.24 km/s
2057-Mar-04 22:12 0.136619 AU
20437861 km
9.21 km/s
2057-Oct-01 16:09 0.182477 AU
27298172 km
6.21 km/s
2078-Mar-20 04:08 0.058520 AU
8754486 km
6.03 km/s
2078-Aug-30 21:04 0.117844 AU
17629272 km
6.33 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
27.24

Orbit Quality

RMS
0.37694
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.