SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 MS3

2026 MS3

2026 MS3 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.901 AU and a period of 0.86 yr.

Aten Observations: 68
Orbital Period · P
0.86 yr
v(q)
46.1 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.04 km
TJ
6.55
Eccentricity · e
0.3676

Orbit and dynamics

Between its closest point (0.57 AU) and its farthest (1.232 AU), the heliocentric distance changes by 0.662 AU over every revolution.

One full revolution takes 0.86 yr (312 days), computed from the semi-major axis of 0.901 AU.

An eccentricity of 0.368 makes the orbit moderately elongated.

Its inclination of 3.66° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 46.1 km/s at perihelion and falls to 21.3 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 = 24.84 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 68 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4562 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
0.9009 AU
Eccentricity
0.3676
Perihelion
0.57 AU
Aphelion
1.232071 AU
Inclination
3.66°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
75.94°

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-Oct-07 13:28 0.079836 AU
11943343 km
11.65 km/s
2032-Jun-28 12:02 0.107975 AU
16152866 km
7.67 km/s
2033-Oct-03 11:37 0.173133 AU
25900311 km
15.18 km/s
2038-Jul-17 09:59 0.180111 AU
26944209 km
7.68 km/s
2062-Sep-13 11:16 0.184862 AU
27655010 km
7.59 km/s
2067-Jun-26 14:28 0.155938 AU
23328036 km
15.05 km/s
2068-Sep-29 10:54 0.132141 AU
19768017 km
7.41 km/s
2073-Jun-23 12:23 0.073271 AU
10961147 km
12.45 km/s
2074-Oct-07 23:21 0.074243 AU
11106586 km
8.96 km/s
2079-Jun-22 19:07 0.018153 AU
2715647 km
10.51 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
24.84

Orbit Quality

RMS
0.45618
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.

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