SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 FN2

2025 FN2

2025 FN2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.895 AU and a period of 0.85 yr.

Aten Observations: 31
Orbital Period · P
0.85 yr
v(q)
47.5 km/s
v(Q)
20.9 km/s
Diameter · ≈
0.03 km
TJ
6.58
Eccentricity · e
0.3881

Orbit and dynamics

The path is an ellipse reaching 0.547 AU from the Sun at perihelion and 1.242 AU at aphelion, a radial span of 0.695 AU.

Applying Kepler's third law to a = 0.895 AU gives an orbital period of 0.85 yr, or about 309 days.

An eccentricity of 0.388 makes the orbit moderately elongated.

Its inclination of 1.47° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 47.5 km/s at perihelion and falls to 20.9 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

No direct size measurement is available; from an absolute magnitude of H = 25.74 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 31 observations and has a weighted RMS residual of 0.3644 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
0.8946 AU
Eccentricity
0.3881
Perihelion
0.547 AU
Aphelion
1.241794 AU
Inclination
1.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
67.97°

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
2034-Dec-10 16:35 0.021841 AU
3267303 km
10.67 km/s
2036-Mar-24 20:37 0.024059 AU
3599220 km
11.58 km/s
2045-Dec-11 09:19 0.005391 AU
806424 km
9.65 km/s
2047-Mar-25 01:45 0.024223 AU
3623721 km
12.78 km/s
2056-Dec-18 16:30 0.127293 AU
19042733 km
8.41 km/s
2058-Mar-22 22:27 0.105224 AU
15741233 km
15.27 km/s
2067-Dec-23 12:06 0.125962 AU
18843699 km
8.37 km/s
2069-Mar-22 09:59 0.090343 AU
13515109 km
15.82 km/s
2078-Dec-17 03:10 0.105215 AU
15739893 km
8.52 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
25.74

Orbit Quality

RMS
0.36442
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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