SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 UK

2015 UK

2015 UK belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.052 AU it takes 1.08 yr to circle the Sun.

Apollo Observations: 21
Orbital Period · P
1.08 yr
v(q)
40.5 km/s
v(Q)
20.8 km/s
Diameter · ≈
0.02 km
TJ
5.8
Eccentricity · e
0.3212

Orbit and dynamics

The path is an ellipse reaching 0.714 AU from the Sun at perihelion and 1.39 AU at aphelion, a radial span of 0.676 AU.

Applying Kepler's third law to a = 1.052 AU gives an orbital period of 1.08 yr, or about 394 days.

An eccentricity of 0.321 makes the orbit moderately elongated.

Its inclination of 3.27° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 40.5 km/s at perihelion and falls to 20.8 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 = 26.4 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 21 observations and has a weighted RMS residual of 0.7799 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
1.052 AU
Eccentricity
0.3212
Perihelion
0.714 AU
Aphelion
1.389902 AU
Inclination
3.27°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
19.81°

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-Oct-17 12:33 0.033524 AU
5015143 km
15.41 km/s
2039-Feb-28 12:32 0.264132 AU
39513659 km
23.73 km/s
2040-Mar-21 04:37 0.022840 AU
3416773 km
8.90 km/s
2042-Oct-05 23:52 0.004468 AU
668377 km
6.47 km/s
2043-Oct-26 02:03 0.222532 AU
33290381 km
21.18 km/s
2053-Mar-08 03:43 0.242000 AU
36202745 km
17.94 km/s
2054-Mar-03 06:14 0.229692 AU
34361423 km
6.12 km/s
2054-Apr-30 15:56 0.219704 AU
32867314 km
7.52 km/s
2055-Jan-06 22:47 0.404366 AU
60492270 km
9.38 km/s
2055-Jul-20 17:37 0.287784 AU
43051927 km
10.64 km/s
2055-Nov-25 11:03 0.330735 AU
49477276 km
8.36 km/s
2056-Oct-11 18:12 0.004362 AU
652486 km
11.33 km/s
2067-Mar-17 05:55 0.021926 AU
3280137 km
12.24 km/s
2070-Oct-21 10:21 0.121370 AU
18156678 km
17.75 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
26.4

Orbit Quality

RMS
0.77986
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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