SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 FN3

2024 FN3

2024 FN3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.024 AU it takes 1.04 yr to circle the Sun.

Apollo Observations: 45
Orbital Period · P
1.04 yr
v(q)
31.2 km/s
v(Q)
27.7 km/s
Diameter · ≈
0.03 km
TJ
5.94
Eccentricity · e
0.0597

Orbit and dynamics

The path is an ellipse reaching 0.963 AU from the Sun at perihelion and 1.085 AU at aphelion, a radial span of 0.122 AU.

Applying Kepler's third law to a = 1.024 AU gives an orbital period of 1.04 yr, or about 378 days.

With e = 0.06, the orbit is close to circular.

The orbital plane is tilted 13.4° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.2 km/s at perihelion and falls to 27.7 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 = 25.35 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 45 observations and has a weighted RMS residual of 0.6456 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
1.024 AU
Eccentricity
0.0597
Perihelion
0.963 AU
Aphelion
1.085133 AU
Inclination
13.4°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
136.02°

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
2049-Sep-17 03:27 0.437521 AU
65452254 km
17.35 km/s
2050-Sep-27 23:30 0.212317 AU
31762152 km
11.64 km/s
2051-Oct-07 16:49 0.011173 AU
1671481 km
7.49 km/s
2052-Apr-08 08:46 0.072848 AU
10897934 km
7.12 km/s
2052-Oct-13 17:48 0.114825 AU
17177534 km
7.84 km/s
2053-Apr-01 20:04 0.068500 AU
10247464 km
7.88 km/s
2053-Oct-13 09:56 0.338762 AU
50678125 km
11.93 km/s
2054-Apr-02 08:09 0.278027 AU
41592308 km
12.15 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
25.35

Orbit Quality

RMS
0.64561
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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