SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 KA2

2013 KA2

2013 KA2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.147 AU it takes 1.23 yr to circle the Sun.

Apollo Observations: 35
Orbital Period · P
1.23 yr
v(q)
50.6 km/s
v(Q)
15.3 km/s
Diameter · ≈
0.22 km
TJ
5.18
Eccentricity · e
0.5365

Orbit and dynamics

The path is an ellipse reaching 0.532 AU from the Sun at perihelion and 1.762 AU at aphelion, a radial span of 1.23 AU.

Applying Kepler's third law to a = 1.147 AU gives an orbital period of 1.23 yr, or about 449 days.

The high eccentricity (0.536) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 35.84° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 50.6 km/s at perihelion and falls to 15.3 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 = 21.09 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

The current orbit solution is based on 35 observations and has a weighted RMS residual of 0.8112 arcseconds.

Condition code U = 1 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
1.147 AU
Eccentricity
0.5365
Perihelion
0.532 AU
Aphelion
1.762366 AU
Inclination
35.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
123.91°

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
2029-Jun-01 08:34 0.411779 AU
61601235 km
18.76 km/s
2031-Jan-02 05:36 0.453626 AU
67861429 km
29.17 km/s
2034-Jun-03 09:40 0.306101 AU
45792108 km
24.39 km/s
2035-Nov-20 22:26 0.415834 AU
62207835 km
29.23 km/s
2045-Jun-03 16:29 0.355099 AU
53122103 km
19.28 km/s
2046-Dec-23 18:17 0.420095 AU
62845365 km
28.72 km/s
2050-Jun-01 06:14 0.352291 AU
52702009 km
26.62 km/s
2051-Nov-12 06:20 0.438080 AU
65535863 km
29.52 km/s
2061-Jun-04 18:38 0.322826 AU
48294093 km
19.88 km/s
2062-Dec-17 09:27 0.405539 AU
60667697 km
28.62 km/s
2066-May-30 13:51 0.392061 AU
58651519 km
28.18 km/s
2067-Nov-06 17:25 0.455154 AU
68090070 km
29.67 km/s
2077-Jun-05 03:56 0.309148 AU
46247954 km
20.31 km/s
2078-Dec-14 03:08 0.400773 AU
59954835 km
28.63 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
21.09

Orbit Quality

RMS
0.81115
Condition
1
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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