SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 DF25

2025 DF25

2025 DF25 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.89 AU and a period of 0.84 yr.

Aten Observations: 22
Orbital Period · P
0.84 yr
v(q)
42.3 km/s
v(Q)
23.5 km/s
Diameter · ≈
0.01 km
TJ
6.64
Eccentricity · e
0.2852

Orbit and dynamics

The path is an ellipse reaching 0.636 AU from the Sun at perihelion and 1.143 AU at aphelion, a radial span of 0.507 AU.

Applying Kepler's third law to a = 0.89 AU gives an orbital period of 0.84 yr, or about 307 days.

An eccentricity of 0.285 makes the orbit moderately elongated.

Its inclination of 0.21° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.3 km/s at perihelion and falls to 23.5 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 = 29.06 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 22 observations and has a weighted RMS residual of 0.5618 arcseconds.

Condition code U = 6 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
0.8897 AU
Eccentricity
0.2852
Perihelion
0.636 AU
Aphelion
1.143442 AU
Inclination
0.21°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
290.33°

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
2030-Feb-28 00:20 0.190498 AU
28498030 km
13.79 km/s
2036-Jun-05 10:10 0.048984 AU
7327848 km
9.42 km/s
2041-May-27 10:53 0.071068 AU
10631591 km
5.85 km/s
2046-Apr-20 01:54 0.136551 AU
20427669 km
6.08 km/s
2051-Mar-13 20:21 0.094900 AU
14196794 km
5.75 km/s
2056-Feb-24 10:32 0.025558 AU
3823378 km
8.78 km/s
2062-Jun-02 22:17 0.181765 AU
27191619 km
13.25 km/s
2067-Jun-04 09:58 0.020640 AU
3087760 km
6.75 km/s
2072-Apr-06 12:41 0.135420 AU
20258512 km
6.08 km/s
2077-Feb-23 04:39 0.039582 AU
5921435 km
8.96 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
29.06

Orbit Quality

RMS
0.56179
Condition
6
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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