SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 FP2

2024 FP2

2024 FP2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.97 AU and a period of 0.96 yr.

Aten Observations: 129
Orbital Period · P
0.96 yr
v(q)
39.2 km/s
v(Q)
23.4 km/s
Diameter · ≈
0.2 km
TJ
6.08
Eccentricity · e
0.2526

Orbit and dynamics

Between its closest point (0.725 AU) and its farthest (1.215 AU), the heliocentric distance changes by 0.49 AU over every revolution.

One full revolution takes 0.96 yr (349 days), computed from the semi-major axis of 0.97 AU.

An eccentricity of 0.253 makes the orbit moderately elongated.

A steep inclination of 31.1° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.2 km/s at perihelion and falls to 23.4 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 = 21.29 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

Astrometry from 129 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4449 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
0.9701 AU
Eccentricity
0.2526
Perihelion
0.725 AU
Aphelion
1.215147 AU
Inclination
31.1°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
321.24°

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
2046-Apr-22 06:42 0.127903 AU
19134006 km
15.78 km/s
2047-Apr-21 18:02 0.171918 AU
25718601 km
18.89 km/s
2067-Apr-21 02:13 0.196000 AU
29321129 km
15.41 km/s
2068-Apr-22 01:47 0.105894 AU
15841498 km
17.46 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
21.29

Orbit Quality

RMS
0.4449
Condition
1
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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