SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 MF2

2024 MF2

2024 MF2 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.847 AU once every 2.51 yr.

Amor Observations: 36
Orbital Period · P
2.51 yr
v(q)
32.7 km/s
v(Q)
14.7 km/s
Diameter · ≈
0.06 km
TJ
3.92
Eccentricity · e
0.3807

Orbit and dynamics

Between its closest point (1.144 AU) and its farthest (2.55 AU), the heliocentric distance changes by 1.406 AU over every revolution.

One full revolution takes 2.51 yr (917 days), computed from the semi-major axis of 1.847 AU.

An eccentricity of 0.381 makes the orbit moderately elongated.

Its inclination of 2.46° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.7 km/s at perihelion and falls to 14.7 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.71 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 36 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5719 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
1.847 AU
Eccentricity
0.3807
Perihelion
1.144 AU
Aphelion
2.550153 AU
Inclination
2.46°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
278.65°

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-Jul-06 18:48 0.127262 AU
19038052 km
3.67 km/s
2034-Jul-13 03:27 0.183886 AU
27509015 km
5.52 km/s
2039-Jul-20 04:57 0.311965 AU
46669346 km
9.26 km/s
2044-May-13 01:07 0.462885 AU
69246645 km
1.85 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
23.71

Orbit Quality

RMS
0.57189
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.

Keep exploring

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