SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 FN1

2024 FN1

2024 FN1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.974 AU and a period of 0.96 yr.

Aten Observations: 22
Orbital Period · P
0.96 yr
v(q)
35 km/s
v(Q)
26.1 km/s
Diameter · ≈
0.02 km
TJ
6.19
Eccentricity · e
0.1453

Orbit and dynamics

The path is an ellipse reaching 0.832 AU from the Sun at perihelion and 1.116 AU at aphelion, a radial span of 0.284 AU.

Applying Kepler's third law to a = 0.974 AU gives an orbital period of 0.96 yr, or about 351 days.

An eccentricity of 0.145 makes the orbit moderately elongated.

The orbital plane is tilted 9.55° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35 km/s at perihelion and falls to 26.1 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 = 26.1 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 22 observations and has a weighted RMS residual of 0.4759 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
0.974 AU
Eccentricity
0.1453
Perihelion
0.832 AU
Aphelion
1.115522 AU
Inclination
9.55°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
357.92°

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
2044-Nov-24 18:47 0.433581 AU
64862798 km
18.40 km/s
2045-Nov-11 03:26 0.212132 AU
31734432 km
11.45 km/s
2046-Oct-14 07:40 0.103170 AU
15434002 km
6.65 km/s
2047-Aug-23 07:26 0.187627 AU
28068635 km
6.92 km/s
2048-Feb-22 09:43 0.153094 AU
22902553 km
5.62 km/s
2048-Jun-19 12:27 0.219818 AU
32884367 km
4.77 km/s
2049-Mar-30 00:42 0.042582 AU
6370187 km
7.20 km/s
2050-Mar-27 22:35 0.246713 AU
36907790 km
13.43 km/s
2069-Nov-18 11:16 0.280918 AU
42024748 km
14.55 km/s
2070-Oct-30 15:01 0.108867 AU
16286292 km
8.07 km/s
2073-Mar-22 21:53 0.053049 AU
7935994 km
5.82 km/s
2074-Mar-30 08:04 0.122618 AU
18343399 km
10.68 km/s
2075-Mar-23 19:53 0.354372 AU
53013331 km
17.46 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
26.1

Orbit Quality

RMS
0.47589
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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