SpaceAtlas Space Object Data
NASA JPL SBDB · 2006 KC

2006 KC

2006 KC belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.221 AU it takes 1.35 yr to circle the Sun.

Apollo Observations: 77
Orbital Period · P
1.35 yr
v(q)
45.1 km/s
v(Q)
16.1 km/s
Diameter · ≈
0.13 km
TJ
5.09
Eccentricity · e
0.4736

Orbit and dynamics

Between its closest point (0.643 AU) and its farthest (1.799 AU), the heliocentric distance changes by 1.156 AU over every revolution.

One full revolution takes 1.35 yr (493 days), computed from the semi-major axis of 1.221 AU.

The high eccentricity (0.474) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.47° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 45.1 km/s at perihelion and falls to 16.1 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 = 22.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

Astrometry from 77 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5073 arcseconds.

Condition code U = 6 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
1.221 AU
Eccentricity
0.4736
Perihelion
0.643 AU
Aphelion
1.799266 AU
Inclination
14.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
3.65°

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
2033-May-05 02:20 0.058014 AU
8678722 km
11.73 km/s
2037-May-17 03:39 0.030120 AU
4505852 km
19.10 km/s
2039-Oct-10 19:29 0.346218 AU
51793534 km
28.71 km/s
2041-May-30 04:49 0.294870 AU
44111979 km
27.22 km/s
2043-Oct-25 14:08 0.091963 AU
13757410 km
20.41 km/s
2060-May-02 10:55 0.183971 AU
27521721 km
9.40 km/s
2064-May-12 05:26 0.029980 AU
4484933 km
16.13 km/s
2068-May-25 16:03 0.227280 AU
34000597 km
24.42 km/s
2070-Oct-20 20:34 0.174925 AU
26168448 km
22.94 km/s
2074-Nov-07 14:57 0.078332 AU
11718374 km
14.66 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
22.2

Orbit Quality

RMS
0.50732
Condition
6
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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