SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 DS8

2026 DS8

2026 DS8 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1 AU it takes 1.00 yr to circle the Sun.

Apollo Observations: 30
Orbital Period · P
1.00 yr
v(q)
39.3 km/s
v(Q)
22.5 km/s
Diameter · ≈
0.02 km
TJ
5.93
Eccentricity · e
0.2715

Orbit and dynamics

The path is an ellipse reaching 0.729 AU from the Sun at perihelion and 1.272 AU at aphelion, a radial span of 0.543 AU.

Applying Kepler's third law to a = 1 AU gives an orbital period of 1.00 yr, or about 365 days.

An eccentricity of 0.272 makes the orbit moderately elongated.

A steep inclination of 30.76° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.3 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

No direct size measurement is available; from an absolute magnitude of H = 26.43 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 30 observations and has a weighted RMS residual of 0.365 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
1.0 AU
Eccentricity
0.2715
Perihelion
0.729 AU
Aphelion
1.2715 AU
Inclination
30.76°
Orbital Period
— yr
Epoch
2461095.5
Mean Anomaly
279.33°

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-Feb-26 09:34 0.033519 AU
5014397 km
17.49 km/s
2028-Feb-26 17:49 0.033649 AU
5033839 km
17.42 km/s
2029-Feb-26 02:51 0.033987 AU
5084376 km
17.32 km/s
2030-Feb-26 12:46 0.034681 AU
5188247 km
17.21 km/s
2031-Feb-26 23:19 0.036003 AU
5385999 km
17.06 km/s
2032-Feb-27 10:53 0.038242 AU
5720890 km
16.89 km/s
2033-Feb-26 22:24 0.041466 AU
6203253 km
16.72 km/s
2034-Feb-27 10:28 0.046570 AU
6966844 km
16.52 km/s
2035-Feb-27 22:16 0.053424 AU
7992102 km
16.33 km/s
2036-Feb-28 08:31 0.062173 AU
9300983 km
16.14 km/s
2037-Feb-27 18:27 0.072827 AU
10894724 km
15.96 km/s
2038-Feb-28 02:21 0.084893 AU
12699810 km
15.82 km/s
2039-Feb-28 08:22 0.098233 AU
14695498 km
15.68 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
26.43

Orbit Quality

RMS
0.36498
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.

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