SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 SP2

2024 SP2

2024 SP2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.931 AU and a period of 0.90 yr.

Aten Observations: 22
Orbital Period · P
0.90 yr
v(q)
35.3 km/s
v(Q)
27 km/s
Diameter · ≈
0.01 km
TJ
6.43
Eccentricity · e
0.1344

Orbit and dynamics

The path is an ellipse reaching 0.806 AU from the Sun at perihelion and 1.056 AU at aphelion, a radial span of 0.25 AU.

Applying Kepler's third law to a = 0.931 AU gives an orbital period of 0.90 yr, or about 328 days.

An eccentricity of 0.134 makes the orbit moderately elongated.

Its inclination of 2.47° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.3 km/s at perihelion and falls to 27 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 = 28.99 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 22 observations and has a weighted RMS residual of 0.6491 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
0.9308 AU
Eccentricity
0.1344
Perihelion
0.806 AU
Aphelion
1.0559 AU
Inclination
2.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
87.95°

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-Oct-02 11:04 0.479763 AU
71771483 km
18.78 km/s
2033-Aug-02 19:00 0.134993 AU
20194597 km
2.61 km/s
2033-Nov-15 02:27 0.072000 AU
10770981 km
3.23 km/s
2034-Feb-16 10:18 0.119153 AU
17824975 km
2.72 km/s
2041-Sep-27 15:23 0.354518 AU
53035197 km
15.07 km/s
2042-Jun-22 20:47 0.184765 AU
27640524 km
4.88 km/s
2043-Jan-06 12:40 0.041810 AU
6254685 km
4.16 km/s
2050-Sep-21 20:19 0.140234 AU
20978696 km
9.25 km/s
2051-May-09 22:53 0.205486 AU
30740266 km
5.93 km/s
2052-Jan-02 21:14 0.182955 AU
27369619 km
10.54 km/s
2060-Mar-20 20:20 0.156981 AU
23484032 km
4.75 km/s
2060-Dec-22 03:16 0.439056 AU
65681868 km
17.63 km/s
2067-Sep-23 22:59 0.010682 AU
1597986 km
11.44 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
28.99

Orbit Quality

RMS
0.64912
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.

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