SpaceAtlas Space Object Data
NASA JPL SBDB · 2025 DS1

2025 DS1

2025 DS1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.887 AU and a period of 0.84 yr.

Aten Observations: 24
Orbital Period · P
0.84 yr
v(q)
36.1 km/s
v(Q)
27.7 km/s
TJ
6.68
Eccentricity · e
0.1314

Orbit and dynamics

The path is an ellipse reaching 0.771 AU from the Sun at perihelion and 1.004 AU at aphelion, a radial span of 0.233 AU.

Applying Kepler's third law to a = 0.887 AU gives an orbital period of 0.84 yr, or about 305 days.

An eccentricity of 0.131 makes the orbit moderately elongated.

Its inclination of 2.37° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.1 km/s at perihelion and falls to 27.7 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 DS1, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 24 observations and has a weighted RMS residual of 0.4223 arcseconds.

Condition code U = 5 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
0.8872 AU
Eccentricity
0.1314
Perihelion
0.771 AU
Aphelion
1.003778 AU
Inclination
2.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
49.05°

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-Jan-04 06:26 0.031518 AU
4714979 km
3.03 km/s
2034-Dec-21 11:37 0.139745 AU
20905541 km
7.57 km/s
2051-Mar-02 16:45 0.170962 AU
25575552 km
8.89 km/s
2056-Feb-21 19:52 0.002900 AU
433884 km
3.35 km/s
2062-Feb-28 17:27 0.138585 AU
20731972 km
8.04 km/s
2078-Dec-10 20:28 0.080331 AU
12017399 km
6.12 km/s
2079-May-20 20:50 0.183363 AU
27430696 km
4.23 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
30.32

Orbit Quality

RMS
0.4223
Condition
5
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.