SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 EX1

2025 EX1

2025 EX1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.166 AU it takes 1.26 yr to circle the Sun.

Apollo Observations: 55
Orbital Period · P
1.26 yr
v(q)
33.9 km/s
v(Q)
22.5 km/s
TJ
5.39
Eccentricity · e
0.2028

Orbit and dynamics

The path is an ellipse reaching 0.93 AU from the Sun at perihelion and 1.402 AU at aphelion, a radial span of 0.472 AU.

Applying Kepler's third law to a = 1.166 AU gives an orbital period of 1.26 yr, or about 460 days.

An eccentricity of 0.203 makes the orbit moderately elongated.

Its inclination of 0.45° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.9 km/s at perihelion and falls to 22.5 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 EX1, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 55 observations and has a weighted RMS residual of 0.2989 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
1.166 AU
Eccentricity
0.2028
Perihelion
0.93 AU
Aphelion
1.402465 AU
Inclination
0.45°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
324.65°

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
2030-Jun-17 18:06 0.033160 AU
4960652 km
4.19 km/s
2035-Jul-13 08:46 0.142111 AU
21259543 km
9.60 km/s
2059-Feb-27 01:09 0.052529 AU
7858258 km
7.38 km/s
2064-Apr-08 22:37 0.065479 AU
9795531 km
4.15 km/s
2069-Jun-25 21:26 0.013296 AU
1989100 km
4.75 km/s
2074-Jul-03 21:30 0.018022 AU
2696071 km
6.16 km/s
2079-Jul-16 04:48 0.181838 AU
27202570 km
11.03 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
30.76

Orbit Quality

RMS
0.29885
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

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