SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 XK16

2012 XK16

2012 XK16 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.169 AU it takes 1.26 yr to circle the Sun.

Apollo Observations: 180
Orbital Period · P
1.26 yr
v(q)
33.3 km/s
v(Q)
22.8 km/s
Diameter · ≈
0.11 km
TJ
5.31
Eccentricity · e
0.1884

Orbit and dynamics

The path is an ellipse reaching 0.949 AU from the Sun at perihelion and 1.389 AU at aphelion, a radial span of 0.44 AU.

Applying Kepler's third law to a = 1.169 AU gives an orbital period of 1.26 yr, or about 462 days.

An eccentricity of 0.188 makes the orbit moderately elongated.

A steep inclination of 23.38° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 33.3 km/s at perihelion and falls to 22.8 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 = 22.52 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 180 observations and has a weighted RMS residual of 0.438 arcseconds.

Condition code U = 3 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
1.169 AU
Eccentricity
0.1884
Perihelion
0.949 AU
Aphelion
1.38924 AU
Inclination
23.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
297.58°

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
2031-Jun-18 08:52 0.202312 AU
30265435 km
13.98 km/s
2031-Dec-05 08:00 0.302091 AU
45192236 km
12.32 km/s
2036-Jun-09 13:27 0.234120 AU
35023890 km
11.80 km/s
2036-Dec-03 23:08 0.071337 AU
10671870 km
13.55 km/s
2041-May-20 05:58 0.433203 AU
64806286 km
11.63 km/s
2041-Dec-13 04:39 0.370226 AU
55384947 km
19.90 km/s
2050-Jun-16 05:23 0.412745 AU
61745711 km
19.06 km/s
2055-Jun-18 01:38 0.182642 AU
27322795 km
13.42 km/s
2055-Dec-03 23:30 0.255697 AU
38251678 km
12.19 km/s
2060-Jun-07 02:41 0.264003 AU
39494231 km
11.75 km/s
2060-Dec-05 03:14 0.103347 AU
15460440 km
14.30 km/s
2065-May-15 05:10 0.465665 AU
69662492 km
11.51 km/s
2065-Dec-15 08:35 0.430183 AU
64354429 km
21.38 km/s
2074-Jun-17 12:09 0.351126 AU
52527680 km
17.55 km/s
2074-Dec-23 17:55 0.490762 AU
73416940 km
12.37 km/s
2079-Jun-16 20:58 0.169615 AU
25373983 km
12.66 km/s
2079-Dec-03 02:28 0.180260 AU
26966512 km
12.16 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
22.52

Orbit Quality

RMS
0.43805
Condition
3
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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