SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 RB4

2026 RB4

2026 RB4 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.769 AU and a period of 0.67 yr.

Aten Observations: 76
Orbital Period · P
0.67 yr
v(q)
52.6 km/s
v(Q)
21.9 km/s
Diameter · ≈
0.02 km
TJ
7.46
Eccentricity · e
0.4117

Orbit and dynamics

Between its closest point (0.452 AU) and its farthest (1.085 AU), the heliocentric distance changes by 0.633 AU over every revolution.

One full revolution takes 0.67 yr (246 days), computed from the semi-major axis of 0.769 AU.

The high eccentricity (0.412) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.81° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 52.6 km/s at perihelion and falls to 21.9 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 = 26.34 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 76 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6742 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
0.7689 AU
Eccentricity
0.4117
Perihelion
0.452 AU
Aphelion
1.085456 AU
Inclination
7.81°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
351.61°

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
2028-Sep-06 01:26 0.085266 AU
12755621 km
12.79 km/s
2051-Nov-05 05:56 0.145140 AU
21712572 km
13.39 km/s
2053-Nov-02 05:45 0.106757 AU
15970581 km
10.06 km/s
2055-Oct-19 03:56 0.109290 AU
16349483 km
8.59 km/s
2057-Sep-28 04:49 0.084744 AU
12677529 km
8.51 km/s
2059-Sep-12 07:43 0.013144 AU
1966248 km
9.28 km/s
2061-Sep-06 13:37 0.030072 AU
4498636 km
11.67 km/s
2063-Sep-07 20:34 0.143792 AU
21510947 km
15.05 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
26.34

Orbit Quality

RMS
0.67422
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.

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