SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 TL2

2024 TL2

2024 TL2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.133 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 35
Orbital Period · P
1.21 yr
v(q)
38.5 km/s
v(Q)
20.3 km/s
TJ
5.48
Eccentricity · e
0.3102

Orbit and dynamics

The path is an ellipse reaching 0.782 AU from the Sun at perihelion and 1.484 AU at aphelion, a radial span of 0.702 AU.

Applying Kepler's third law to a = 1.133 AU gives an orbital period of 1.21 yr, or about 440 days.

An eccentricity of 0.31 makes the orbit moderately elongated.

Its inclination of 2.43° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.5 km/s at perihelion and falls to 20.3 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2024 TL2, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 35 observations and has a weighted RMS residual of 0.3922 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
1.133 AU
Eccentricity
0.3102
Perihelion
0.782 AU
Aphelion
1.484457 AU
Inclination
2.43°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
87.77°

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-Nov-17 11:19 0.154352 AU
23090771 km
6.63 km/s
2031-May-25 23:48 0.399989 AU
59837454 km
7.99 km/s
2036-Aug-23 23:00 0.315943 AU
47264372 km
6.73 km/s
2036-Dec-31 18:09 0.204719 AU
30625561 km
8.29 km/s
2037-May-04 22:02 0.306800 AU
45896651 km
6.58 km/s
2042-Aug-04 14:41 0.393143 AU
58813412 km
8.02 km/s
2048-Jul-18 23:23 0.443032 AU
66276698 km
8.72 km/s
2049-Mar-26 02:18 0.005915 AU
884799 km
9.32 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
30.76

Orbit Quality

RMS
0.3922
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

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