SpaceAtlas Space Object Data
NASA JPL SBDB · 2009 KW2

2009 KW2

2009 KW2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.362 AU it takes 1.59 yr to circle the Sun.

Apollo Observations: 62
Orbital Period · P
1.59 yr
v(q)
33.1 km/s
v(Q)
19.7 km/s
Diameter · ≈
0.02 km
TJ
4.81
Eccentricity · e
0.2537

Orbit and dynamics

Between its closest point (1.016 AU) and its farthest (1.708 AU), the heliocentric distance changes by 0.692 AU over every revolution.

One full revolution takes 1.59 yr (581 days), computed from the semi-major axis of 1.362 AU.

An eccentricity of 0.254 makes the orbit moderately elongated.

The orbital plane is tilted 5.19° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.1 km/s at perihelion and falls to 19.7 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 62 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3732 arcseconds.

Condition code U = 5 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
1.362 AU
Eccentricity
0.2537
Perihelion
1.016 AU
Aphelion
1.707539 AU
Inclination
5.19°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
258.96°

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
2028-Feb-20 05:48 0.423148 AU
63302081 km
5.55 km/s
2028-Jul-24 01:50 0.359006 AU
53706514 km
14.88 km/s
2036-Jun-19 18:25 0.045056 AU
6740345 km
5.42 km/s
2044-Apr-25 22:09 0.115797 AU
17322941 km
7.55 km/s
2052-Apr-06 01:51 0.372826 AU
55773980 km
15.64 km/s
2052-Sep-09 19:41 0.430307 AU
64372954 km
5.57 km/s
2063-Feb-20 00:56 0.412263 AU
61673663 km
5.59 km/s
2063-Jul-25 13:43 0.336990 AU
50413058 km
15.04 km/s
2071-Jul-03 07:26 0.067996 AU
10172091 km
7.13 km/s
2079-May-07 21:41 0.020684 AU
3094312 km
5.65 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
26.6

Orbit Quality

RMS
0.37316
Condition
5
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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