SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 EZ26

2016 EZ26

2016 EZ26 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.436 AU it takes 3.80 yr to circle the Sun.

Apollo Observations: 102
Orbital Period · P
3.80 yr
v(q)
37.9 km/s
v(Q)
9.6 km/s
Diameter · ≈
0.11 km
TJ
3.23
Eccentricity · e
0.5948

Orbit and dynamics

The path is an ellipse reaching 0.987 AU from the Sun at perihelion and 3.885 AU at aphelion, a radial span of 2.898 AU.

Applying Kepler's third law to a = 2.436 AU gives an orbital period of 3.80 yr, or about 1,389 days.

The high eccentricity (0.595) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.82° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37.9 km/s at perihelion and falls to 9.6 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

The measured diameter is 0.27 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.022 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 102 observations and has a weighted RMS residual of 0.5922 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
2.436 AU
Eccentricity
0.5948
Perihelion
0.987 AU
Aphelion
3.884933 AU
Inclination
6.82°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
238.05°

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
2035-Apr-26 17:19 0.059071 AU
8836965 km
9.29 km/s
2054-Jun-22 03:30 0.176057 AU
26337707 km
15.31 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.268 km
Albedo
0.022
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
22.6

Orbit Quality

RMS
0.59221
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.

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