SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 FN3

2026 FN3

2026 FN3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.046 AU it takes 1.07 yr to circle the Sun.

Apollo Observations: 58
Orbital Period · P
1.07 yr
v(q)
38 km/s
v(Q)
22.3 km/s
Diameter · ≈
0.02 km
TJ
5.84
Eccentricity · e
0.2603

Orbit and dynamics

The path is an ellipse reaching 0.774 AU from the Sun at perihelion and 1.318 AU at aphelion, a radial span of 0.544 AU.

Applying Kepler's third law to a = 1.046 AU gives an orbital period of 1.07 yr, or about 391 days.

An eccentricity of 0.26 makes the orbit moderately elongated.

Its inclination of 1.83° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38 km/s at perihelion and falls to 22.3 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 = 26.73 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 58 observations and has a weighted RMS residual of 0.477 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
1.046 AU
Eccentricity
0.2603
Perihelion
0.774 AU
Aphelion
1.318274 AU
Inclination
1.83°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
140.92°

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
2038-Sep-01 11:48 0.109862 AU
16435086 km
11.68 km/s
2041-Mar-12 08:52 0.050784 AU
7597223 km
4.77 km/s
2056-Jan-11 23:15 0.186642 AU
27921206 km
6.95 km/s
2057-Mar-25 16:49 0.145907 AU
21827378 km
12.62 km/s
2069-Sep-07 12:37 0.010669 AU
1596039 km
7.90 km/s
2072-Mar-17 10:47 0.004867 AU
728074 km
6.87 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
26.73

Orbit Quality

RMS
0.47703
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.

Keep exploring

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