SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 FG

2024 FG

2024 FG belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.317 AU it takes 1.51 yr to circle the Sun.

Apollo Observations: 33
Orbital Period · P
1.51 yr
v(q)
37.6 km/s
v(Q)
17.9 km/s
Diameter · ≈
0.05 km
TJ
4.89
Eccentricity · e
0.3551

Orbit and dynamics

The path is an ellipse reaching 0.85 AU from the Sun at perihelion and 1.785 AU at aphelion, a radial span of 0.935 AU.

Applying Kepler's third law to a = 1.317 AU gives an orbital period of 1.51 yr, or about 552 days.

An eccentricity of 0.355 makes the orbit moderately elongated.

Its inclination of 3.78° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.6 km/s at perihelion and falls to 17.9 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 = 24.06 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

The current orbit solution is based on 33 observations and has a weighted RMS residual of 0.3528 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
1.317 AU
Eccentricity
0.3551
Perihelion
0.85 AU
Aphelion
1.784667 AU
Inclination
3.78°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
123.48°

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-May-09 06:15 0.134958 AU
20189394 km
7.33 km/s
2027-Oct-01 13:06 0.438774 AU
65639719 km
6.79 km/s
2030-Jun-18 18:28 0.175892 AU
26313112 km
8.30 km/s
2033-Feb-26 07:20 0.438984 AU
65671020 km
7.26 km/s
2033-Jul-30 17:13 0.106411 AU
15918874 km
7.23 km/s
2036-Aug-25 11:06 0.021042 AU
3147785 km
10.32 km/s
2039-Sep-07 05:07 0.143697 AU
21496736 km
15.89 km/s
2042-Sep-16 18:15 0.317286 AU
47465349 km
21.72 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
24.06

Orbit Quality

RMS
0.35283
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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