SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 KF

2015 KF

2015 KF is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.98 AU and a period of 0.97 yr.

Aten Observations: 56
Orbital Period · P
0.97 yr
v(q)
34.8 km/s
v(Q)
26 km/s
Diameter · ≈
0.03 km
TJ
6.16
Eccentricity · e
0.1454

Orbit and dynamics

The path is an ellipse reaching 0.837 AU from the Sun at perihelion and 1.122 AU at aphelion, a radial span of 0.285 AU.

Applying Kepler's third law to a = 0.98 AU gives an orbital period of 0.97 yr, or about 354 days.

An eccentricity of 0.145 makes the orbit moderately elongated.

The orbital plane is tilted 7.47° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34.8 km/s at perihelion and falls to 26 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 = 25.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 56 observations and has a weighted RMS residual of 0.5293 arcseconds.

Condition code U = 2 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
0.9795 AU
Eccentricity
0.1454
Perihelion
0.837 AU
Aphelion
1.121919 AU
Inclination
7.47°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
271.74°

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
2045-May-02 16:03 0.327800 AU
49038218 km
13.70 km/s
2046-Apr-27 20:01 0.148994 AU
22289186 km
8.42 km/s
2047-May-09 05:31 0.058780 AU
8793367 km
4.75 km/s
2048-Jan-09 17:56 0.171180 AU
25608118 km
5.41 km/s
2048-Jun-24 15:59 0.140246 AU
20980433 km
4.50 km/s
2048-Nov-21 03:45 0.129046 AU
19304940 km
5.67 km/s
2049-Oct-04 04:26 0.109216 AU
16338516 km
5.65 km/s
2050-Sep-11 08:42 0.236240 AU
35341050 km
10.21 km/s
2051-Aug-30 16:34 0.412070 AU
61644794 km
15.69 km/s
2076-May-05 04:23 0.403002 AU
60288215 km
15.96 km/s
2077-Apr-28 23:03 0.218680 AU
32714052 km
10.50 km/s
2078-Apr-30 06:05 0.059518 AU
8903707 km
5.68 km/s
2079-Feb-03 14:47 0.172829 AU
25854798 km
4.24 km/s
2079-Jun-04 08:28 0.113285 AU
16947236 km
4.62 km/s
2079-Dec-11 05:42 0.149337 AU
22340450 km
5.83 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
25.1

Orbit Quality

RMS
0.52927
Condition
2
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.

Keep exploring

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