SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 SO2

2024 SO2

2024 SO2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.964 AU and a period of 0.95 yr.

Aten Observations: 24
Orbital Period · P
0.95 yr
v(q)
33.7 km/s
v(Q)
27.3 km/s
Diameter · ≈
0.01 km
TJ
6.25
Eccentricity · e
0.1052

Orbit and dynamics

The path is an ellipse reaching 0.862 AU from the Sun at perihelion and 1.065 AU at aphelion, a radial span of 0.203 AU.

Applying Kepler's third law to a = 0.964 AU gives an orbital period of 0.95 yr, or about 345 days.

An eccentricity of 0.105 makes the orbit moderately elongated.

Its inclination of 4.36° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.7 km/s at perihelion and falls to 27.3 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 = 27.9 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 24 observations and has a weighted RMS residual of 0.4367 arcseconds.

Condition code U = 5 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
0.9635 AU
Eccentricity
0.1052
Perihelion
0.862 AU
Aphelion
1.06486 AU
Inclination
4.36°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
39.82°

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-Jan-22 04:05 0.371066 AU
55510731 km
14.77 km/s
2040-Oct-05 03:05 0.473074 AU
70770826 km
17.92 km/s
2041-Sep-23 10:52 0.141307 AU
21139300 km
8.01 km/s
2042-Jul-04 18:00 0.151439 AU
22654965 km
3.65 km/s
2042-Dec-11 13:30 0.105141 AU
15728867 km
2.88 km/s
2043-Mar-20 02:42 0.101071 AU
15119937 km
3.53 km/s
2044-Jan-28 14:29 0.234299 AU
35050645 km
10.63 km/s
2058-Sep-29 16:23 0.323698 AU
48424576 km
13.37 km/s
2059-Sep-22 12:32 0.005733 AU
857615 km
3.97 km/s
2060-Apr-29 00:03 0.157632 AU
23581402 km
4.63 km/s
2061-Jan-24 12:10 0.153610 AU
22979752 km
8.06 km/s
2073-Sep-22 03:50 0.100972 AU
15105217 km
8.05 km/s
2076-Jan-13 16:38 0.338400 AU
50623894 km
15.53 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
27.9

Orbit Quality

RMS
0.43666
Condition
5
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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