SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 EV2

2025 EV2

2025 EV2 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.582 AU once every 1.99 yr.

Amor Observations: 26
Orbital Period · P
1.99 yr
v(q)
34.3 km/s
v(Q)
16.3 km/s
Diameter · ≈
0.11 km
TJ
4.14
Eccentricity · e
0.355

Orbit and dynamics

The path is an ellipse reaching 1.021 AU from the Sun at perihelion and 2.144 AU at aphelion, a radial span of 1.123 AU.

Applying Kepler's third law to a = 1.582 AU gives an orbital period of 1.99 yr, or about 727 days.

An eccentricity of 0.355 makes the orbit moderately elongated.

A steep inclination of 34.1° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.3 km/s at perihelion and falls to 16.3 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 22.55 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 26 observations and has a weighted RMS residual of 0.5041 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
1.582 AU
Eccentricity
0.355
Perihelion
1.021 AU
Aphelion
2.14361 AU
Inclination
34.1°
Orbital Period
— yr
Epoch
2460742.5
Mean Anomaly
336.69°

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-Mar-14 02:17 0.107147 AU
16028942 km
18.64 km/s
2029-Mar-11 21:30 0.094130 AU
14081642 km
19.01 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
22.55

Orbit Quality

RMS
0.50407
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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