SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 KO

2016 KO

2016 KO is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.817 AU and a period of 0.74 yr.

Aten Observations: 73
Orbital Period · P
0.74 yr
v(q)
45.5 km/s
v(Q)
23.9 km/s
Diameter · ≈
0.02 km
TJ
7.12
Eccentricity · e
0.3113

Orbit and dynamics

The path is an ellipse reaching 0.563 AU from the Sun at perihelion and 1.072 AU at aphelion, a radial span of 0.509 AU.

Applying Kepler's third law to a = 0.817 AU gives an orbital period of 0.74 yr, or about 270 days.

An eccentricity of 0.311 makes the orbit moderately elongated.

The orbital plane is tilted 6.5° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 45.5 km/s at perihelion and falls to 23.9 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 = 26.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 73 observations and has a weighted RMS residual of 0.5887 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
0.8172 AU
Eccentricity
0.3113
Perihelion
0.563 AU
Aphelion
1.071594 AU
Inclination
6.5°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
339.54°

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
2027-Jun-04 13:18 0.435322 AU
65123211 km
21.65 km/s
2027-Dec-07 04:23 0.411786 AU
61602325 km
15.15 km/s
2030-May-25 12:54 0.169273 AU
25322840 km
13.52 km/s
2030-Nov-04 23:50 0.363116 AU
54321398 km
11.99 km/s
2033-May-30 20:18 0.005148 AU
770115 km
6.56 km/s
2036-Mar-09 08:06 0.322600 AU
48260212 km
7.59 km/s
2036-Jul-26 00:16 0.109985 AU
16453578 km
8.53 km/s
2039-Jan-27 16:33 0.403708 AU
60393791 km
13.72 km/s
2039-Jul-21 22:30 0.341473 AU
51083676 km
17.40 km/s
2041-Dec-25 09:04 0.423214 AU
63311983 km
15.68 km/s
2044-May-30 04:03 0.286004 AU
42785664 km
18.06 km/s
2044-Nov-22 12:11 0.391591 AU
58581235 km
14.12 km/s
2047-May-23 13:42 0.005820 AU
870587 km
9.43 km/s
2053-Jul-26 08:27 0.129582 AU
19385207 km
12.78 km/s
2056-Jul-16 13:56 0.357109 AU
53422784 km
21.33 km/s
2061-May-26 18:03 0.124686 AU
18652821 km
14.84 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
26.5

Orbit Quality

RMS
0.5887
Condition
7
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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