SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 FN

2023 FN

2023 FN is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.78 AU and a period of 0.69 yr.

Aten Observations: 32
Orbital Period · P
0.69 yr
v(q)
57.3 km/s
v(Q)
19.9 km/s
Diameter · ≈
0.05 km
TJ
7.32
Eccentricity · e
0.4854

Orbit and dynamics

Between its closest point (0.401 AU) and its farthest (1.158 AU), the heliocentric distance changes by 0.757 AU over every revolution.

One full revolution takes 0.69 yr (251 days), computed from the semi-major axis of 0.78 AU.

The high eccentricity (0.485) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 16.46° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 57.3 km/s at perihelion and falls to 19.9 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 = 24.46 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 32 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5405 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.7796 AU
Eccentricity
0.4854
Perihelion
0.401 AU
Aphelion
1.158018 AU
Inclination
16.46°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
11.73°

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
2030-May-09 16:32 0.266828 AU
39916910 km
16.71 km/s
2032-Apr-11 03:23 0.207753 AU
31079391 km
11.88 km/s
2034-Mar-11 01:16 0.033141 AU
4957852 km
13.89 km/s
2036-Mar-17 12:57 0.264218 AU
39526463 km
24.51 km/s
2039-May-01 15:52 0.405000 AU
60587180 km
26.26 km/s
2041-May-08 23:19 0.243817 AU
36474572 km
14.72 km/s
2045-Mar-10 04:18 0.035756 AU
5349021 km
15.44 km/s
2047-Mar-21 01:58 0.220537 AU
32991851 km
26.79 km/s
2050-May-04 06:07 0.292093 AU
43696487 km
23.83 km/s
2056-Mar-10 22:31 0.043373 AU
6488565 km
17.78 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
24.46

Orbit Quality

RMS
0.54047
Condition
7
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.