SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 XA3

2011 XA3

2011 XA3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.467 AU it takes 1.78 yr to circle the Sun.

Apollo Observations: 156
Orbital Period · P
1.78 yr
v(q)
125.2 km/s
v(Q)
4.8 km/s
Diameter · ≈
0.29 km
TJ
3.9
Eccentricity · e
0.9258

Orbit and dynamics

Between its closest point (0.109 AU) and its farthest (2.825 AU), the heliocentric distance changes by 2.716 AU over every revolution.

One full revolution takes 1.78 yr (649 days), computed from the semi-major axis of 1.467 AU.

The high eccentricity (0.926) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 28.12° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 125.2 km/s at perihelion and falls to 4.8 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 = 20.46 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.29 km.

Observation record and orbit quality

Astrometry from 156 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3645 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
1.467 AU
Eccentricity
0.9258
Perihelion
0.109 AU
Aphelion
2.825149 AU
Inclination
28.12°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
31.29°

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-Dec-19 20:26 0.067810 AU
10144272 km
38.89 km/s
2038-Oct-20 09:45 0.442065 AU
66132042 km
36.79 km/s
2043-Dec-15 09:08 0.166555 AU
24916262 km
42.16 km/s
2051-Jan-03 05:09 0.407147 AU
60908364 km
26.95 km/s
2054-Oct-15 09:08 0.458510 AU
68592167 km
33.47 km/s
2059-Dec-10 13:57 0.269849 AU
40368900 km
45.63 km/s
2067-Jan-01 03:42 0.300080 AU
44891315 km
29.15 km/s
2070-Oct-10 16:40 0.496852 AU
74327933 km
30.38 km/s
2075-Dec-05 22:13 0.366830 AU
54877007 km
49.03 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
20.46

Orbit Quality

RMS
0.36452
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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