SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 FE3

2026 FE3

2026 FE3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.271 AU it takes 1.43 yr to circle the Sun.

Apollo Observations: 178
Orbital Period · P
1.43 yr
v(q)
35.7 km/s
v(Q)
19.6 km/s
Diameter · ≈
0.02 km
TJ
5.04
Eccentricity · e
0.2919

Orbit and dynamics

Between its closest point (0.9 AU) and its farthest (1.642 AU), the heliocentric distance changes by 0.742 AU over every revolution.

One full revolution takes 1.43 yr (523 days), computed from the semi-major axis of 1.271 AU.

An eccentricity of 0.292 makes the orbit moderately elongated.

Its inclination of 2.36° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.7 km/s at perihelion and falls to 19.6 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 = 26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 178 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5243 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
1.271 AU
Eccentricity
0.2919
Perihelion
0.9 AU
Aphelion
1.642005 AU
Inclination
2.36°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
88.82°

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
2048-Nov-20 09:09 0.039986 AU
5981852 km
9.16 km/s
2069-Feb-28 19:20 0.048049 AU
7188023 km
5.32 km/s
2079-Mar-24 03:03 0.028235 AU
4223970 km
8.69 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
26.0

Orbit Quality

RMS
0.52428
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.

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