SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 TO6

2024 TO6

2024 TO6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.345 AU it takes 1.56 yr to circle the Sun.

Apollo Observations: 34
Orbital Period · P
1.56 yr
v(q)
44.8 km/s
v(Q)
14.7 km/s
Diameter · ≈
0.01 km
TJ
4.72
Eccentricity · e
0.5045

Orbit and dynamics

The path is an ellipse reaching 0.666 AU from the Sun at perihelion and 2.024 AU at aphelion, a radial span of 1.358 AU.

Applying Kepler's third law to a = 1.345 AU gives an orbital period of 1.56 yr, or about 570 days.

The high eccentricity (0.504) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 15.56° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.8 km/s at perihelion and falls to 14.7 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 = 27.21 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 34 observations and has a weighted RMS residual of 0.3078 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.345 AU
Eccentricity
0.5045
Perihelion
0.666 AU
Aphelion
2.023553 AU
Inclination
15.56°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
59.7°

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
2032-Apr-07 07:01 0.000233 AU
34846 km
15.97 km/s
2038-Oct-19 23:46 0.085367 AU
12770741 km
24.57 km/s
2043-Mar-16 13:24 0.218488 AU
32685348 km
29.20 km/s
2071-Apr-14 12:06 0.131964 AU
19741500 km
13.42 km/s
2077-Oct-26 00:56 0.245908 AU
36787312 km
28.45 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
27.21

Orbit Quality

RMS
0.30784
Condition
7
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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