SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 YF2

2024 YF2

2024 YF2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.059 AU it takes 1.09 yr to circle the Sun.

Apollo Observations: 65
Orbital Period · P
1.09 yr
v(q)
33.9 km/s
v(Q)
24.7 km/s
Diameter · ≈
0.02 km
TJ
5.8
Eccentricity · e
0.1572

Orbit and dynamics

Between its closest point (0.892 AU) and its farthest (1.225 AU), the heliocentric distance changes by 0.333 AU over every revolution.

One full revolution takes 1.09 yr (398 days), computed from the semi-major axis of 1.059 AU.

An eccentricity of 0.157 makes the orbit moderately elongated.

Its inclination of 1.86° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.9 km/s at perihelion and falls to 24.7 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 = 26.58 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 65 individual observations underpins this orbit; the fit leaves an RMS residual of 0.438 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
1.059 AU
Eccentricity
0.1572
Perihelion
0.892 AU
Aphelion
1.225475 AU
Inclination
1.86°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
44.32°

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
2037-Jan-11 05:07 0.075792 AU
11338366 km
7.04 km/s
2038-Jun-29 18:12 0.061587 AU
9213280 km
6.51 km/s
2049-Jan-08 06:31 0.146378 AU
21897873 km
9.20 km/s
2050-Jun-25 16:15 0.005204 AU
778485 km
4.85 km/s
2060-Jan-20 17:21 0.011194 AU
1674594 km
5.62 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
26.58

Orbit Quality

RMS
0.43796
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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