SpaceAtlas Space Object Data
NASA JPL SBDB · 2026 LR2

2026 LR2

2026 LR2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.125 AU it takes 1.19 yr to circle the Sun.

Apollo Observations: 62
Orbital Period · P
1.19 yr
v(q)
33 km/s
v(Q)
23.9 km/s
Diameter · ≈
0.14 km
TJ
5.49
Eccentricity · e
0.1611

Orbit and dynamics

Between its closest point (0.944 AU) and its farthest (1.306 AU), the heliocentric distance changes by 0.362 AU over every revolution.

One full revolution takes 1.19 yr (436 days), computed from the semi-major axis of 1.125 AU.

An eccentricity of 0.161 makes the orbit moderately elongated.

The orbital plane is tilted 19.07° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33 km/s at perihelion and falls to 23.9 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 = 22.09 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.14 km.

Observation record and orbit quality

Astrometry from 62 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3551 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
1.125 AU
Eccentricity
0.1611
Perihelion
0.944 AU
Aphelion
1.306237 AU
Inclination
19.07°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
233.47°

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-08 07:35 0.195685 AU
29274026 km
11.42 km/s
2032-Sep-01 00:59 0.035333 AU
5285807 km
10.33 km/s
2033-Feb-16 10:56 0.180250 AU
26964994 km
10.27 km/s
2038-Aug-26 02:53 0.102484 AU
15331316 km
12.08 km/s
2075-Sep-04 05:47 0.088524 AU
13242960 km
10.03 km/s
2076-Feb-14 07:45 0.172322 AU
25779053 km
10.45 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
22.09

Orbit Quality

RMS
0.35506
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.