SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 FJ2

2026 FJ2

2026 FJ2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.99 AU and a period of 0.98 yr.

Aten Observations: 26
Orbital Period · P
0.98 yr
v(q)
32.1 km/s
v(Q)
27.9 km/s
TJ
6.12
Eccentricity · e
0.0695

Orbit and dynamics

The path is an ellipse reaching 0.921 AU from the Sun at perihelion and 1.058 AU at aphelion, a radial span of 0.137 AU.

Applying Kepler's third law to a = 0.99 AU gives an orbital period of 0.98 yr, or about 360 days.

With e = 0.07, the orbit is close to circular.

The orbital plane is tilted 7.48° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 32.1 km/s at perihelion and falls to 27.9 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 FJ2, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 26 observations and has a weighted RMS residual of 0.4326 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
0.9896 AU
Eccentricity
0.0695
Perihelion
0.921 AU
Aphelion
1.058377 AU
Inclination
7.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
175.78°

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
2027-Mar-21 03:56 0.093943 AU
14053665 km
4.07 km/s
2027-Sep-27 06:09 0.065394 AU
9782732 km
4.00 km/s
2028-Sep-08 08:17 0.042619 AU
6375694 km
4.62 km/s
2029-Aug-26 08:56 0.139016 AU
20796438 km
6.70 km/s
2076-Mar-21 19:19 0.178577 AU
26714767 km
7.99 km/s
2077-Mar-17 15:09 0.064808 AU
9695069 km
5.28 km/s
2078-Mar-16 07:54 0.032874 AU
4917917 km
3.96 km/s
2078-Oct-12 20:34 0.105560 AU
15791600 km
4.09 km/s
2079-Apr-06 17:15 0.145306 AU
21737501 km
4.53 km/s
2079-Sep-12 13:38 0.033165 AU
4961452 km
4.30 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
30.44

Orbit Quality

RMS
0.43262
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.

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