SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 TX2

2024 TX2

2024 TX2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.044 AU it takes 1.07 yr to circle the Sun.

Apollo Observations: 56
Orbital Period · P
1.07 yr
v(q)
38.7 km/s
v(Q)
21.9 km/s
Diameter · ≈
0.06 km
TJ
5.77
Eccentricity · e
0.277

Orbit and dynamics

Between its closest point (0.755 AU) and its farthest (1.333 AU), the heliocentric distance changes by 0.578 AU over every revolution.

One full revolution takes 1.07 yr (390 days), computed from the semi-major axis of 1.044 AU.

An eccentricity of 0.277 makes the orbit moderately elongated.

A steep inclination of 24.02° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.7 km/s at perihelion and falls to 21.9 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 = 23.86 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 56 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3569 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
1.044 AU
Eccentricity
0.277
Perihelion
0.755 AU
Aphelion
1.333188 AU
Inclination
24.02°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
118.18°

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-Apr-20 06:29 0.105496 AU
15781997 km
15.48 km/s
2028-May-15 02:15 0.421990 AU
63128801 km
23.69 km/s
2039-Oct-06 20:18 0.336276 AU
50306245 km
22.75 km/s
2040-Oct-17 19:15 0.049473 AU
7401083 km
14.06 km/s
2041-Oct-02 12:54 0.348619 AU
52152729 km
12.17 km/s
2043-Apr-17 13:51 0.102878 AU
15390385 km
15.01 km/s
2044-May-13 04:51 0.333573 AU
49901796 km
22.87 km/s
2055-Oct-06 04:28 0.251681 AU
37650993 km
23.21 km/s
2056-Oct-17 14:35 0.049610 AU
7421536 km
14.31 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
23.86

Orbit Quality

RMS
0.35687
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.