SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 WZ1

2016 WZ1

2016 WZ1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.83 AU it takes 2.48 yr to circle the Sun.

Apollo Observations: 104
Orbital Period · P
2.48 yr
v(q)
46.4 km/s
v(Q)
10.4 km/s
Diameter · ≈
0.49 km
TJ
3.74
Eccentricity · e
0.6326

Orbit and dynamics

The path is an ellipse reaching 0.672 AU from the Sun at perihelion and 2.988 AU at aphelion, a radial span of 2.316 AU.

Applying Kepler's third law to a = 1.83 AU gives an orbital period of 2.48 yr, or about 904 days.

The high eccentricity (0.633) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.34° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 46.4 km/s at perihelion and falls to 10.4 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 = 19.31 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.49 km.

Observation record and orbit quality

The current orbit solution is based on 104 observations and has a weighted RMS residual of 0.5317 arcseconds.

Condition code U = 0 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
1.83 AU
Eccentricity
0.6326
Perihelion
0.672 AU
Aphelion
2.987658 AU
Inclination
13.34°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
253.08°

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-Feb-09 02:17 0.291501 AU
43607882 km
15.55 km/s
2032-Jan-01 19:44 0.234978 AU
35152172 km
19.50 km/s
2036-Dec-14 01:51 0.438039 AU
65529668 km
29.09 km/s
2054-Jul-07 09:56 0.475039 AU
71064750 km
30.20 km/s
2059-Jun-19 05:23 0.244454 AU
36569795 km
21.21 km/s
2064-May-09 20:12 0.271637 AU
40636302 km
16.18 km/s
2069-Mar-24 20:43 0.329881 AU
49349538 km
18.72 km/s
2074-Feb-10 20:03 0.294489 AU
44054972 km
15.77 km/s
2078-Dec-31 19:45 0.241032 AU
36057914 km
20.08 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
19.31

Orbit Quality

RMS
0.53172
Condition
0
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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