SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 CJ

2024 CJ

2024 CJ belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.133 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 32
Orbital Period · P
1.21 yr
v(q)
36.1 km/s
v(Q)
21.7 km/s
Diameter · ≈
0.03 km
TJ
5.5
Eccentricity · e
0.2501

Orbit and dynamics

The path is an ellipse reaching 0.85 AU from the Sun at perihelion and 1.416 AU at aphelion, a radial span of 0.566 AU.

Applying Kepler's third law to a = 1.133 AU gives an orbital period of 1.21 yr, or about 440 days.

An eccentricity of 0.25 makes the orbit moderately elongated.

Its inclination of 3.57° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.1 km/s at perihelion and falls to 21.7 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 = 25.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 32 observations and has a weighted RMS residual of 0.3233 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
1.133 AU
Eccentricity
0.2501
Perihelion
0.85 AU
Aphelion
1.416363 AU
Inclination
3.57°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
33.33°

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
2029-Jun-04 00:53 0.383402 AU
57356193 km
7.53 km/s
2030-Feb-05 14:27 0.118008 AU
17653799 km
11.73 km/s
2034-Aug-06 16:24 0.341669 AU
51112914 km
18.92 km/s
2035-May-18 02:06 0.406168 AU
60761922 km
7.82 km/s
2036-Feb-16 04:54 0.279275 AU
41779003 km
17.62 km/s
2040-Aug-15 08:51 0.124758 AU
18663467 km
13.40 km/s
2041-Apr-30 17:55 0.394943 AU
59082601 km
7.72 km/s
2046-Aug-25 22:09 0.042491 AU
6356629 km
8.04 km/s
2064-Jun-30 23:09 0.291650 AU
43630267 km
6.35 km/s
2070-Jun-16 03:36 0.356820 AU
53379505 km
7.11 km/s
2071-Jan-29 05:55 0.013918 AU
2082131 km
7.95 km/s
2076-May-26 07:59 0.396517 AU
59318123 km
7.75 km/s
2077-Feb-11 05:24 0.179953 AU
26920537 km
14.85 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
25.2

Orbit Quality

RMS
0.32333
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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