SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 VV2

2025 VV2

2025 VV2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.736 AU and a period of 0.63 yr.

Aten Observations: 30
Orbital Period · P
0.63 yr
v(q)
54 km/s
v(Q)
22.3 km/s
Diameter · ≈
0.03 km
TJ
7.75
Eccentricity · e
0.4163

Orbit and dynamics

Between its closest point (0.43 AU) and its farthest (1.043 AU), the heliocentric distance changes by 0.613 AU over every revolution.

One full revolution takes 0.63 yr (231 days), computed from the semi-major axis of 0.736 AU.

The high eccentricity (0.416) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.55° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 54 km/s at perihelion and falls to 22.3 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

No direct size measurement is available; from an absolute magnitude of H = 25.43 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 30 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4094 arcseconds.

Condition code U = 8 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.7363 AU
Eccentricity
0.4163
Perihelion
0.43 AU
Aphelion
1.042822 AU
Inclination
7.55°
Orbital Period
— yr
Epoch
2460990.5
Mean Anomaly
152.19°

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
2049-Oct-29 02:52 0.147076 AU
22002315 km
15.90 km/s
2051-Dec-17 21:12 0.135062 AU
20205022 km
11.95 km/s
2056-Oct-29 16:18 0.008061 AU
1205845 km
10.14 km/s
2070-Dec-10 01:37 0.092976 AU
13908986 km
9.04 km/s
2075-Oct-28 19:55 0.085699 AU
12820358 km
14.37 km/s
2077-Dec-18 00:57 0.112364 AU
16809355 km
13.02 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
25.43

Orbit Quality

RMS
0.40938
Condition
8
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.