SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 CZ31

2016 CZ31

2016 CZ31 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.438 AU it takes 1.72 yr to circle the Sun.

Apollo Observations: 71
Orbital Period · P
1.72 yr
v(q)
42.4 km/s
v(Q)
14.6 km/s
Diameter · ≈
0.14 km
TJ
4.51
Eccentricity · e
0.4881

Orbit and dynamics

The path is an ellipse reaching 0.736 AU from the Sun at perihelion and 2.14 AU at aphelion, a radial span of 1.404 AU.

Applying Kepler's third law to a = 1.438 AU gives an orbital period of 1.72 yr, or about 630 days.

The high eccentricity (0.488) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.58° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 42.4 km/s at perihelion and falls to 14.6 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 = 22.07 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.14 km.

Observation record and orbit quality

The current orbit solution is based on 71 observations and has a weighted RMS residual of 0.4714 arcseconds.

Condition code U = 2 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
1.438 AU
Eccentricity
0.4881
Perihelion
0.736 AU
Aphelion
2.139888 AU
Inclination
14.58°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
55.48°

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-Jan-15 20:45 0.181839 AU
27202711 km
19.58 km/s
2034-Oct-16 01:24 0.333655 AU
49914057 km
12.73 km/s
2035-Jan-20 05:51 0.480546 AU
71888634 km
9.63 km/s
2041-Jul-22 08:13 0.118767 AU
17767270 km
18.65 km/s
2047-Jan-09 21:54 0.103136 AU
15428987 km
15.81 km/s
2053-Sep-20 02:11 0.298050 AU
44587631 km
12.18 km/s
2060-Jul-15 07:19 0.247175 AU
36976893 km
22.14 km/s
2066-Jan-04 14:20 0.148321 AU
22188522 km
12.66 km/s
2072-Aug-25 22:23 0.226936 AU
33949163 km
11.23 km/s
2078-Jan-26 09:50 0.406373 AU
60792553 km
26.65 km/s
2079-Jul-10 11:30 0.358109 AU
53572413 km
25.22 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
22.07

Orbit Quality

RMS
0.47145
Condition
2
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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