SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 WY

2016 WY

2016 WY is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.849 AU and a period of 0.78 yr.

Aten Observations: 34
Orbital Period · P
0.78 yr
v(q)
38.4 km/s
v(Q)
27.2 km/s
Diameter · ≈
0.01 km
TJ
6.93
Eccentricity · e
0.17

Orbit and dynamics

The path is an ellipse reaching 0.705 AU from the Sun at perihelion and 0.993 AU at aphelion, a radial span of 0.288 AU.

Applying Kepler's third law to a = 0.849 AU gives an orbital period of 0.78 yr, or about 286 days.

An eccentricity of 0.17 makes the orbit moderately elongated.

Its inclination of 1.96° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.4 km/s at perihelion and falls to 27.2 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 29.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 34 observations and has a weighted RMS residual of 0.4416 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
0.8489 AU
Eccentricity
0.17
Perihelion
0.705 AU
Aphelion
0.993213 AU
Inclination
1.96°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
268.35°

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
2027-Jun-21 03:17 0.296332 AU
44330679 km
8.41 km/s
2027-Dec-12 19:57 0.433931 AU
64915186 km
17.64 km/s
2030-Oct-29 04:18 0.224771 AU
33625261 km
11.36 km/s
2031-Mar-28 05:30 0.250698 AU
37503829 km
6.56 km/s
2034-Aug-01 12:57 0.231932 AU
34696500 km
5.56 km/s
2034-Dec-21 04:49 0.172387 AU
25788731 km
9.92 km/s
2037-Nov-05 23:43 0.451388 AU
67526635 km
19.16 km/s
2038-May-07 03:30 0.299583 AU
44817030 km
8.80 km/s
2048-Oct-23 22:14 0.013565 AU
2029299 km
7.59 km/s
2066-Dec-17 17:33 0.026578 AU
3975939 km
4.43 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
29.2

Orbit Quality

RMS
0.44159
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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