SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 VB1

2025 VB1

2025 VB1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.535 AU it takes 1.90 yr to circle the Sun.

Apollo Observations: 36
Orbital Period · P
1.90 yr
v(q)
50.5 km/s
v(Q)
11.4 km/s
Diameter · ≈
0.02 km
TJ
4.23
Eccentricity · e
0.6304

Orbit and dynamics

The path is an ellipse reaching 0.567 AU from the Sun at perihelion and 2.503 AU at aphelion, a radial span of 1.936 AU.

Applying Kepler's third law to a = 1.535 AU gives an orbital period of 1.90 yr, or about 695 days.

The high eccentricity (0.63) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 0.43° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 50.5 km/s at perihelion and falls to 11.4 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 = 26.36 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 36 observations and has a weighted RMS residual of 0.3785 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
1.535 AU
Eccentricity
0.6304
Perihelion
0.567 AU
Aphelion
2.502664 AU
Inclination
0.43°
Orbital Period
— yr
Epoch
2460990.5
Mean Anomaly
26.97°

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
2063-Nov-18 23:43 0.021439 AU
3207290 km
25.65 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
26.36

Orbit Quality

RMS
0.37847
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

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