SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 LG

2024 LG

2024 LG belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.354 AU it takes 3.61 yr to circle the Sun.

Apollo Observations: 107
Orbital Period · P
3.61 yr
v(q)
38.2 km/s
v(Q)
9.9 km/s
Diameter · ≈
0.2 km
TJ
3.27
Eccentricity · e
0.5891

Orbit and dynamics

The path is an ellipse reaching 0.967 AU from the Sun at perihelion and 3.741 AU at aphelion, a radial span of 2.774 AU.

Applying Kepler's third law to a = 2.354 AU gives an orbital period of 3.61 yr, or about 1,319 days.

The high eccentricity (0.589) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 12.14° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 38.2 km/s at perihelion and falls to 9.9 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 = 21.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

The current orbit solution is based on 107 observations and has a weighted RMS residual of 0.3809 arcseconds.

Condition code U = 4 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
2.354 AU
Eccentricity
0.5891
Perihelion
0.967 AU
Aphelion
3.740741 AU
Inclination
12.14°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
184.75°

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
2042-Aug-18 07:31 0.122290 AU
18294251 km
10.62 km/s
2060-Jul-27 22:51 0.171322 AU
25629362 km
10.42 km/s
2078-Aug-19 09:09 0.110050 AU
16463299 km
10.72 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
21.3

Orbit Quality

RMS
0.38092
Condition
4
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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