SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 AR26

2011 AR26

2011 AR26 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.355 AU it takes 1.58 yr to circle the Sun.

Apollo Observations: 125
Orbital Period · P
1.58 yr
v(q)
39.3 km/s
v(Q)
16.7 km/s
Diameter · ≈
0.31 km
TJ
4.69
Eccentricity · e
0.4044

Orbit and dynamics

Between its closest point (0.807 AU) and its farthest (1.903 AU), the heliocentric distance changes by 1.096 AU over every revolution.

One full revolution takes 1.58 yr (576 days), computed from the semi-major axis of 1.355 AU.

The high eccentricity (0.404) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 24.32° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.3 km/s at perihelion and falls to 16.7 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 = 20.28 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.31 km.

Observation record and orbit quality

Astrometry from 125 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6463 arcseconds.

Condition code U = 0 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
1.355 AU
Eccentricity
0.4044
Perihelion
0.807 AU
Aphelion
1.902962 AU
Inclination
24.32°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
359.42°

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
2029-Jun-23 14:56 0.431567 AU
64561574 km
25.64 km/s
2032-Oct-01 22:41 0.396053 AU
59248736 km
14.12 km/s
2032-Dec-27 06:56 0.354586 AU
53045336 km
13.69 km/s
2040-Jul-09 04:04 0.208099 AU
31131163 km
20.06 km/s
2043-Dec-24 07:45 0.338733 AU
50673810 km
16.96 km/s
2051-Jul-29 05:53 0.115855 AU
17331643 km
16.32 km/s
2054-Dec-29 04:36 0.463378 AU
69320327 km
22.96 km/s
2062-Aug-26 23:51 0.277736 AU
41548725 km
15.34 km/s
2063-Jan-05 09:55 0.441836 AU
66097797 km
13.50 km/s
2070-Jun-27 01:45 0.382807 AU
57267153 km
24.41 km/s
2073-Dec-26 01:55 0.338101 AU
50579231 km
14.05 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
20.28

Orbit Quality

RMS
0.64626
Condition
0
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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