SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 RT34

2026 RT34

2026 RT34 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.021 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 40
Orbital Period · P
1.03 yr
v(q)
44.7 km/s
v(Q)
19.4 km/s
TJ
5.91
Eccentricity · e
0.3945

Orbit and dynamics

The path is an ellipse reaching 0.618 AU from the Sun at perihelion and 1.424 AU at aphelion, a radial span of 0.806 AU.

Applying Kepler's third law to a = 1.021 AU gives an orbital period of 1.03 yr, or about 377 days.

An eccentricity of 0.395 makes the orbit moderately elongated.

Its inclination of 0.67° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.7 km/s at perihelion and falls to 19.4 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 2026 RT34, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 40 observations and has a weighted RMS residual of 0.2846 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
1.021 AU
Eccentricity
0.3945
Perihelion
0.618 AU
Aphelion
1.423785 AU
Inclination
0.67°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
202.49°

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
2035-May-16 12:23 0.108544 AU
16237936 km
13.92 km/s
2038-Sep-07 13:55 0.169302 AU
25327212 km
16.89 km/s
2047-May-14 10:16 0.131074 AU
19608413 km
8.07 km/s
2049-Sep-13 06:14 0.064019 AU
9577084 km
9.29 km/s
2058-May-18 16:10 0.149620 AU
22382875 km
15.66 km/s
2061-Sep-09 11:14 0.113130 AU
16924023 km
15.29 km/s
2070-May-12 15:57 0.103813 AU
15530217 km
9.24 km/s
2072-Sep-10 12:51 0.119761 AU
17916042 km
8.37 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
30.36

Orbit Quality

RMS
0.28463
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

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