SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 XN55

2012 XN55

2012 XN55 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.749 AU and a period of 0.65 yr.

Aten Observations: 68
Orbital Period · P
0.65 yr
v(q)
56.2 km/s
v(Q)
21.1 km/s
Diameter · ≈
0.06 km
TJ
7.54
Eccentricity · e
0.454

Orbit and dynamics

Between its closest point (0.409 AU) and its farthest (1.088 AU), the heliocentric distance changes by 0.679 AU over every revolution.

One full revolution takes 0.65 yr (237 days), computed from the semi-major axis of 0.749 AU.

The high eccentricity (0.454) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 29.08° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 56.2 km/s at perihelion and falls to 21.1 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 = 23.87 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 68 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4522 arcseconds.

Condition code U = 2 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
0.7486 AU
Eccentricity
0.454
Perihelion
0.409 AU
Aphelion
1.088464 AU
Inclination
29.08°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
89.1°

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-31 22:30 0.394360 AU
58995455 km
20.01 km/s
2032-Dec-06 20:25 0.356725 AU
53365299 km
25.05 km/s
2034-Dec-04 00:02 0.091917 AU
13750568 km
17.43 km/s
2036-Dec-15 01:11 0.175400 AU
26239522 km
15.62 km/s
2038-Dec-30 10:53 0.354763 AU
53071840 km
18.66 km/s
2043-Dec-09 12:38 0.416434 AU
62297638 km
26.99 km/s
2045-Dec-03 09:05 0.137100 AU
20509942 km
18.61 km/s
2047-Dec-12 11:15 0.137701 AU
20599786 km
15.56 km/s
2049-Dec-28 00:12 0.315123 AU
47141793 km
17.53 km/s
2054-Dec-11 11:20 0.478028 AU
71511970 km
29.03 km/s
2056-Dec-03 10:56 0.190906 AU
28559116 km
20.07 km/s
2058-Dec-09 05:32 0.100525 AU
15038285 km
15.69 km/s
2060-Dec-24 20:43 0.277714 AU
41545406 km
16.71 km/s
2063-Jan-01 03:41 0.478945 AU
71649203 km
23.24 km/s
2067-Dec-05 01:44 0.245793 AU
36770163 km
21.65 km/s
2069-Dec-06 16:16 0.072371 AU
10826546 km
16.03 km/s
2071-Dec-22 12:27 0.243753 AU
36464959 km
16.18 km/s
2074-Jan-01 04:04 0.435471 AU
65145516 km
21.53 km/s
2078-Dec-06 00:21 0.298357 AU
44633608 km
23.24 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
23.87

Orbit Quality

RMS
0.45221
Condition
2
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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