SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 PF2

2025 PF2

2025 PF2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.992 AU and a period of 0.99 yr.

Aten Observations: 27
Orbital Period · P
0.99 yr
v(q)
44 km/s
v(Q)
20.3 km/s
TJ
6.06
Eccentricity · e
0.3674

Orbit and dynamics

The path is an ellipse reaching 0.627 AU from the Sun at perihelion and 1.356 AU at aphelion, a radial span of 0.729 AU.

Applying Kepler's third law to a = 0.992 AU gives an orbital period of 0.99 yr, or about 361 days.

An eccentricity of 0.367 makes the orbit moderately elongated.

The orbital plane is tilted 5.78° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44 km/s at perihelion and falls to 20.3 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2025 PF2, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 27 observations and has a weighted RMS residual of 0.4262 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
0.9916 AU
Eccentricity
0.3674
Perihelion
0.627 AU
Aphelion
1.355914 AU
Inclination
5.78°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
9.78°

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
2027-Aug-16 16:57 0.151364 AU
22643803 km
7.72 km/s
2042-Jan-04 04:22 0.133018 AU
19899193 km
7.77 km/s
2043-Jan-02 05:15 0.075943 AU
11360880 km
10.12 km/s
2043-Dec-30 08:38 0.070006 AU
10472720 km
12.47 km/s
2044-Dec-26 05:15 0.115976 AU
17349692 km
14.90 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
30.13

Orbit Quality

RMS
0.42621
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.

Keep exploring

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