SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 TO2

2024 TO2

2024 TO2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.064 AU it takes 1.10 yr to circle the Sun.

Apollo Observations: 48
Orbital Period · P
1.10 yr
v(q)
33 km/s
v(Q)
25.3 km/s
Diameter · ≈
0.02 km
TJ
5.67
Eccentricity · e
0.1325

Orbit and dynamics

Between its closest point (0.923 AU) and its farthest (1.205 AU), the heliocentric distance changes by 0.282 AU over every revolution.

One full revolution takes 1.10 yr (401 days), computed from the semi-major axis of 1.064 AU.

An eccentricity of 0.133 makes the orbit moderately elongated.

A steep inclination of 29.15° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 33 km/s at perihelion and falls to 25.3 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

No direct size measurement is available; from an absolute magnitude of H = 26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 48 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4966 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
1.064 AU
Eccentricity
0.1325
Perihelion
0.923 AU
Aphelion
1.20498 AU
Inclination
29.15°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
119.06°

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
2035-Oct-03 11:59 0.011172 AU
1671333 km
16.34 km/s
2036-Mar-30 04:15 0.184422 AU
27589124 km
15.47 km/s
2036-Oct-09 11:42 0.323103 AU
48335559 km
17.50 km/s
2037-Apr-05 15:50 0.121146 AU
18123118 km
18.56 km/s
2046-Sep-29 02:04 0.000183 AU
27357 km
18.44 km/s
2047-Apr-02 10:41 0.220045 AU
32918260 km
16.64 km/s
2047-Oct-10 23:18 0.101109 AU
15125692 km
15.96 km/s
2048-Apr-02 04:44 0.047369 AU
7086349 km
16.41 km/s
2059-Mar-31 18:34 0.056597 AU
8466846 km
15.17 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
26.0

Orbit Quality

RMS
0.49662
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.

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