SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 EL2

2026 EL2

2026 EL2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.913 AU and a period of 0.87 yr.

Aten Observations: 154
Orbital Period · P
0.87 yr
v(q)
34.8 km/s
v(Q)
28 km/s
Diameter · ≈
0.02 km
TJ
6.53
Eccentricity · e
0.1084

Orbit and dynamics

Between its closest point (0.814 AU) and its farthest (1.012 AU), the heliocentric distance changes by 0.198 AU over every revolution.

One full revolution takes 0.87 yr (319 days), computed from the semi-major axis of 0.913 AU.

An eccentricity of 0.108 makes the orbit moderately elongated.

Its inclination of 0.63° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.8 km/s at perihelion and falls to 28 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 = 26.15 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 154 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3337 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
0.9129 AU
Eccentricity
0.1084
Perihelion
0.814 AU
Aphelion
1.011858 AU
Inclination
0.63°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
258.62°

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-Nov-27 03:15 0.142746 AU
21354521 km
3.26 km/s
2033-Apr-30 00:07 0.086472 AU
12936060 km
5.04 km/s
2039-Oct-06 03:01 0.187586 AU
28062539 km
5.04 km/s
2046-Aug-18 11:54 0.177760 AU
26592526 km
4.47 km/s
2053-Feb-15 17:14 0.022851 AU
3418490 km
2.92 km/s
2053-Jun-19 14:55 0.109250 AU
16343562 km
1.49 km/s
2060-Feb-15 23:28 0.187589 AU
28062970 km
8.31 km/s
2060-Aug-20 01:20 0.169199 AU
25311838 km
4.27 km/s
2067-Oct-07 21:40 0.178089 AU
26641723 km
4.78 km/s
2074-Nov-30 06:35 0.130831 AU
19572006 km
3.10 km/s
2075-May-04 00:10 0.056454 AU
8445404 km
4.51 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
26.15

Orbit Quality

RMS
0.3337
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.

Keep exploring

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