SpaceAtlas Space Object Data
NASA JPL SBDB · 2006 KS1

2006 KS1

2006 KS1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.471 AU it takes 1.78 yr to circle the Sun.

Apollo Observations: 54
Orbital Period · P
1.78 yr
v(q)
34 km/s
v(Q)
17.7 km/s
Diameter · ≈
0.03 km
TJ
4.55
Eccentricity · e
0.3148

Orbit and dynamics

The path is an ellipse reaching 1.008 AU from the Sun at perihelion and 1.934 AU at aphelion, a radial span of 0.926 AU.

Applying Kepler's third law to a = 1.471 AU gives an orbital period of 1.78 yr, or about 652 days.

An eccentricity of 0.315 makes the orbit moderately elongated.

Its inclination of 3.65° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34 km/s at perihelion and falls to 17.7 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 25.41 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 54 observations and has a weighted RMS residual of 0.793 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
1.471 AU
Eccentricity
0.3148
Perihelion
1.008 AU
Aphelion
1.934071 AU
Inclination
3.65°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
117.38°

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-Feb-18 09:56 0.402447 AU
60205187 km
16.64 km/s
2031-Jul-14 03:27 0.478643 AU
71603981 km
5.15 km/s
2038-Jan-17 10:57 0.442869 AU
66252233 km
5.11 km/s
2038-Jun-07 14:39 0.333270 AU
49856469 km
14.80 km/s
2047-Mar-12 21:57 0.109133 AU
16326029 km
7.30 km/s
2063-May-09 07:00 0.032579 AU
4873817 km
5.63 km/s
2072-Feb-25 14:20 0.293962 AU
43976084 km
13.32 km/s
2072-Jun-29 17:37 0.408755 AU
61148944 km
3.41 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
25.41

Orbit Quality

RMS
0.79301
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.

Keep exploring

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