SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 YU2

2018 YU2

2018 YU2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.083 AU it takes 1.13 yr to circle the Sun.

Apollo Observations: 33
Orbital Period · P
1.13 yr
v(q)
33.3 km/s
v(Q)
24.6 km/s
Diameter · ≈
0.02 km
TJ
5.71
Eccentricity · e
0.1517

Orbit and dynamics

The path is an ellipse reaching 0.919 AU from the Sun at perihelion and 1.247 AU at aphelion, a radial span of 0.328 AU.

Applying Kepler's third law to a = 1.083 AU gives an orbital period of 1.13 yr, or about 412 days.

An eccentricity of 0.152 makes the orbit moderately elongated.

Its inclination of 2.75° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.3 km/s at perihelion and falls to 24.6 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 = 26.5 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 33 observations and has a weighted RMS residual of 0.4344 arcseconds.

Condition code U = 6 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
1.083 AU
Eccentricity
0.1517
Perihelion
0.919 AU
Aphelion
1.247291 AU
Inclination
2.75°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
158.29°

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
2028-Feb-15 09:28 0.067788 AU
10140977 km
3.12 km/s
2028-Jul-21 22:59 0.173786 AU
25998030 km
3.62 km/s
2036-Nov-17 03:09 0.180459 AU
26996264 km
3.81 km/s
2037-May-03 19:27 0.065431 AU
9788278 km
2.89 km/s
2044-Dec-16 16:48 0.489164 AU
73177906 km
18.96 km/s
2045-Oct-28 18:00 0.217157 AU
32486260 km
4.50 km/s
2046-Jun-01 21:11 0.029715 AU
4445304 km
4.77 km/s
2053-Dec-29 23:27 0.232459 AU
34775445 km
11.30 km/s
2054-Sep-16 00:47 0.250627 AU
37493326 km
5.10 km/s
2055-Jun-17 14:20 0.291300 AU
43577924 km
12.78 km/s
2063-Jan-22 21:38 0.035492 AU
5309553 km
3.13 km/s
2063-Jul-28 05:38 0.188190 AU
28152778 km
3.91 km/s
2070-Dec-21 17:58 0.404589 AU
60525652 km
16.58 km/s
2071-Oct-11 11:13 0.242547 AU
36284468 km
4.99 km/s
2072-Jun-08 02:19 0.130787 AU
19565420 km
8.24 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
0.43436
Condition
6
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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