SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 CF3

2024 CF3

2024 CF3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.154 AU it takes 1.24 yr to circle the Sun.

Apollo Observations: 15
Orbital Period · P
1.24 yr
v(q)
34.1 km/s
v(Q)
22.5 km/s
Diameter · ≈
0.02 km
TJ
5.43
Eccentricity · e
0.2049

Orbit and dynamics

Between its closest point (0.917 AU) and its farthest (1.39 AU), the heliocentric distance changes by 0.473 AU over every revolution.

One full revolution takes 1.24 yr (453 days), computed from the semi-major axis of 1.154 AU.

An eccentricity of 0.205 makes the orbit moderately elongated.

Its inclination of 1.09° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.1 km/s at perihelion and falls to 22.5 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 = 26.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 15 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3858 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
1.154 AU
Eccentricity
0.2049
Perihelion
0.917 AU
Aphelion
1.390455 AU
Inclination
1.09°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
4.97°

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
2028-Oct-02 10:31 0.013927 AU
2083432 km
5.43 km/s
2029-Mar-26 22:04 0.236193 AU
35334025 km
4.49 km/s
2033-Sep-06 11:22 0.379588 AU
56785516 km
17.47 km/s
2034-May-15 22:30 0.357487 AU
53479283 km
6.67 km/s
2040-Feb-20 11:15 0.196334 AU
29371079 km
15.51 km/s
2049-Sep-16 00:01 0.098874 AU
14791413 km
11.90 km/s
2055-Jun-11 10:21 0.361751 AU
54117162 km
6.69 km/s
2056-Feb-27 07:12 0.490384 AU
73360330 km
19.69 km/s
2065-Sep-28 08:05 0.053038 AU
7934428 km
6.71 km/s
2066-Apr-03 14:08 0.265671 AU
39743867 km
4.94 km/s
2070-Sep-04 08:13 0.396383 AU
59298068 km
19.09 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
26.3

Orbit Quality

RMS
0.3858
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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