SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 XP

2025 XP

2025 XP is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.912 AU and a period of 0.87 yr.

Aten Observations: 61
Orbital Period · P
0.87 yr
v(q)
48.9 km/s
v(Q)
19.9 km/s
Diameter · ≈
0.01 km
TJ
6.46
Eccentricity · e
0.4223

Orbit and dynamics

Between its closest point (0.527 AU) and its farthest (1.297 AU), the heliocentric distance changes by 0.77 AU over every revolution.

One full revolution takes 0.87 yr (318 days), computed from the semi-major axis of 0.912 AU.

The high eccentricity (0.422) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.87° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 48.9 km/s at perihelion and falls to 19.9 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 = 27.29 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 61 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4173 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
0.9122 AU
Eccentricity
0.4223
Perihelion
0.527 AU
Aphelion
1.297422 AU
Inclination
3.87°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
285.91°

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
2032-Dec-15 08:05 0.173596 AU
25969665 km
9.18 km/s
2041-Mar-25 07:05 0.065107 AU
9739827 km
12.59 km/s
2045-Dec-11 22:33 0.165855 AU
24811579 km
18.67 km/s
2052-Dec-06 06:35 0.009414 AU
1408297 km
12.17 km/s
2061-Mar-23 23:21 0.115147 AU
17225762 km
9.89 km/s
2068-Mar-21 11:50 0.096375 AU
14417444 km
16.65 km/s
2072-Dec-07 00:21 0.005186 AU
775852 km
13.67 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
27.29

Orbit Quality

RMS
0.41735
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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