SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 ES1

2026 ES1

2026 ES1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.266 AU it takes 1.42 yr to circle the Sun.

Apollo Observations: 22
Orbital Period · P
1.42 yr
v(q)
38 km/s
v(Q)
18.4 km/s
TJ
5.02
Eccentricity · e
0.3478

Orbit and dynamics

Between its closest point (0.826 AU) and its farthest (1.706 AU), the heliocentric distance changes by 0.88 AU over every revolution.

One full revolution takes 1.42 yr (520 days), computed from the semi-major axis of 1.266 AU.

An eccentricity of 0.348 makes the orbit moderately elongated.

The orbital plane is tilted 10.11° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 38 km/s at perihelion and falls to 18.4 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 ES1, so its physical size remains unconstrained.

Observation record and orbit quality

Astrometry from 22 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4064 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.266 AU
Eccentricity
0.3478
Perihelion
0.826 AU
Aphelion
1.706315 AU
Inclination
10.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
100.19°

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
2055-Oct-12 09:01 0.102751 AU
15371396 km
10.70 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
30.11

Orbit Quality

RMS
0.40643
Condition
7
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.