SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 KT1

2013 KT1

2013 KT1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.923 AU and a period of 0.89 yr.

Aten Observations: 111
Orbital Period · P
0.89 yr
v(q)
36.6 km/s
v(Q)
26.3 km/s
Diameter · ≈
0.02 km
TJ
6.46
Eccentricity · e
0.1643

Orbit and dynamics

The path is an ellipse reaching 0.771 AU from the Sun at perihelion and 1.075 AU at aphelion, a radial span of 0.304 AU.

Applying Kepler's third law to a = 0.923 AU gives an orbital period of 0.89 yr, or about 324 days.

An eccentricity of 0.164 makes the orbit moderately elongated.

The orbital plane is tilted 8.11° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 36.6 km/s at perihelion and falls to 26.3 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 = 26.6 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 111 observations and has a weighted RMS residual of 0.2627 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
0.9231 AU
Eccentricity
0.1643
Perihelion
0.771 AU
Aphelion
1.074765 AU
Inclination
8.11°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
135.17°

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
2036-Jan-28 16:14 0.144106 AU
21557978 km
7.23 km/s
2044-Jan-06 01:50 0.131591 AU
19685743 km
5.40 km/s
2051-Dec-10 08:54 0.159442 AU
23852201 km
6.24 km/s
2052-Apr-28 17:09 0.098478 AU
14732134 km
4.79 km/s
2059-Nov-25 20:51 0.182568 AU
27311762 km
6.84 km/s
2060-May-15 02:06 0.054349 AU
8130487 km
4.97 km/s
2067-Nov-27 18:23 0.178732 AU
26737937 km
6.75 km/s
2068-May-12 02:16 0.066067 AU
9883519 km
4.88 km/s
2075-Dec-13 19:41 0.152331 AU
22788456 km
6.07 km/s
2076-Apr-19 03:43 0.116636 AU
17448517 km
4.79 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
0.26274
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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