SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 KE

2015 KE

2015 KE is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.974 AU and a period of 0.96 yr.

Aten Observations: 110
Orbital Period · P
0.96 yr
v(q)
34.2 km/s
v(Q)
26.6 km/s
Diameter · ≈
0.02 km
TJ
6.2
Eccentricity · e
0.1244

Orbit and dynamics

The path is an ellipse reaching 0.853 AU from the Sun at perihelion and 1.095 AU at aphelion, a radial span of 0.242 AU.

Applying Kepler's third law to a = 0.974 AU gives an orbital period of 0.96 yr, or about 351 days.

An eccentricity of 0.124 makes the orbit moderately elongated.

Its inclination of 0.62° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.2 km/s at perihelion and falls to 26.6 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 = 26.2 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 110 observations and has a weighted RMS residual of 0.4163 arcseconds.

Condition code U = 3 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
0.9737 AU
Eccentricity
0.1244
Perihelion
0.853 AU
Aphelion
1.094828 AU
Inclination
0.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
302.2°

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
2039-May-03 00:53 0.106192 AU
15886165 km
6.29 km/s
2040-Feb-27 06:54 0.106672 AU
15957965 km
2.94 km/s
2040-Jun-29 03:32 0.077593 AU
11607798 km
2.64 km/s
2040-Dec-06 23:46 0.119534 AU
17882016 km
3.48 km/s
2041-Sep-17 16:46 0.064593 AU
9662981 km
5.04 km/s
2063-May-02 01:01 0.064514 AU
9651131 km
5.10 km/s
2064-Feb-11 06:12 0.119255 AU
17840266 km
3.45 km/s
2064-Jul-19 00:21 0.078013 AU
11670593 km
2.66 km/s
2064-Nov-21 04:43 0.106608 AU
15948365 km
3.00 km/s
2065-Sep-16 14:11 0.104958 AU
15701559 km
6.26 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
26.2

Orbit Quality

RMS
0.41629
Condition
3
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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