SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 FP10

2025 FP10

2025 FP10 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.776 AU and a period of 0.68 yr.

Aten Observations: 156
Orbital Period · P
0.68 yr
v(q)
44.4 km/s
v(Q)
25.7 km/s
Diameter · ≈
0.59 km
TJ
7.36
Eccentricity · e
0.266

Orbit and dynamics

Between its closest point (0.57 AU) and its farthest (0.983 AU), the heliocentric distance changes by 0.413 AU over every revolution.

One full revolution takes 0.68 yr (250 days), computed from the semi-major axis of 0.776 AU.

An eccentricity of 0.266 makes the orbit moderately elongated.

A steep inclination of 27.84° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 44.4 km/s at perihelion and falls to 25.7 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 18.89 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.59 km.

Observation record and orbit quality

Astrometry from 156 individual observations underpins this orbit; the fit leaves an RMS residual of 0.343 arcseconds.

Condition code U = 2 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
0.7765 AU
Eccentricity
0.266
Perihelion
0.57 AU
Aphelion
0.983049 AU
Inclination
27.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
48.77°

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
2038-Apr-12 12:23 0.028800 AU
4308348 km
14.00 km/s
2051-Apr-13 00:32 0.044945 AU
6723688 km
14.16 km/s
2064-Apr-12 22:33 0.096855 AU
14489343 km
14.68 km/s
2075-Apr-12 08:17 0.141422 AU
21156419 km
14.29 km/s
2077-Apr-14 07:20 0.165660 AU
24782388 km
15.66 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
18.89

Orbit Quality

RMS
0.34299
Condition
2
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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