SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 WL2

2018 WL2

2018 WL2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.884 AU and a period of 0.83 yr.

Aten Observations: 62
Orbital Period · P
0.83 yr
v(q)
72.1 km/s
v(Q)
13.9 km/s
Diameter · ≈
0.15 km
TJ
6.39
Eccentricity · e
0.6766

Orbit and dynamics

The path is an ellipse reaching 0.286 AU from the Sun at perihelion and 1.482 AU at aphelion, a radial span of 1.196 AU.

Applying Kepler's third law to a = 0.884 AU gives an orbital period of 0.83 yr, or about 303 days.

The high eccentricity (0.677) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 34.94° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 72.1 km/s at perihelion and falls to 13.9 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 = 21.86 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.15 km.

Observation record and orbit quality

The current orbit solution is based on 62 observations and has a weighted RMS residual of 0.4648 arcseconds.

Condition code U = 1 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
0.8837 AU
Eccentricity
0.6766
Perihelion
0.286 AU
Aphelion
1.481611 AU
Inclination
34.94°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
293.53°

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-Dec-03 17:21 0.089521 AU
13392205 km
24.32 km/s
2033-Dec-02 08:12 0.096563 AU
14445689 km
26.29 km/s
2038-Nov-30 06:28 0.155708 AU
23293578 km
28.56 km/s
2043-Nov-27 14:36 0.233274 AU
34897258 km
31.10 km/s
2047-Nov-22 18:04 0.480782 AU
71923896 km
19.84 km/s
2048-Nov-23 12:26 0.316351 AU
47325369 km
33.80 km/s
2052-Nov-25 11:05 0.434083 AU
64937939 km
19.84 km/s
2053-Nov-20 04:41 0.399475 AU
59760556 km
36.56 km/s
2057-Nov-28 23:10 0.380011 AU
56848819 km
19.93 km/s
2058-Nov-16 16:01 0.482822 AU
72229137 km
39.43 km/s
2062-Dec-02 01:32 0.318523 AU
47650393 km
20.20 km/s
2067-Dec-04 09:32 0.252454 AU
37766572 km
20.78 km/s
2072-Dec-04 16:42 0.184329 AU
27575192 km
21.75 km/s
2077-Dec-04 20:44 0.120295 AU
17995889 km
23.17 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
21.86

Orbit Quality

RMS
0.4648
Condition
1
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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