SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 RA2

2026 RA2

2026 RA2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.888 AU and a period of 0.84 yr.

Aten Observations: 39
Orbital Period · P
0.84 yr
v(q)
64 km/s
v(Q)
15.6 km/s
Diameter · ≈
0.04 km
TJ
6.51
Eccentricity · e
0.608

Orbit and dynamics

Between its closest point (0.348 AU) and its farthest (1.428 AU), the heliocentric distance changes by 1.08 AU over every revolution.

One full revolution takes 0.84 yr (306 days), computed from the semi-major axis of 0.888 AU.

The high eccentricity (0.608) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.04° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 64 km/s at perihelion and falls to 15.6 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 = 24.88 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 39 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3582 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
0.8881 AU
Eccentricity
0.608
Perihelion
0.348 AU
Aphelion
1.428065 AU
Inclination
6.04°
Orbital Period
— yr
Epoch
2461290.5
Mean Anomaly
77.39°

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
2031-Sep-04 17:47 0.016581 AU
2480433 km
21.15 km/s
2038-Nov-28 13:06 0.102232 AU
15293657 km
19.82 km/s
2043-Nov-30 23:53 0.099012 AU
14812023 km
16.24 km/s
2062-Sep-01 14:02 0.008885 AU
1329231 km
15.35 km/s
2067-Sep-02 04:48 0.011124 AU
1664053 km
17.88 km/s
2072-Sep-03 07:06 0.024929 AU
3729370 km
20.18 km/s
2077-Sep-06 12:16 0.091887 AU
13746120 km
23.00 km/s
2079-Nov-26 07:43 0.114800 AU
17173804 km
22.41 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
24.88

Orbit Quality

RMS
0.3582
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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