SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 UZ40

2016 UZ40

2016 UZ40 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.072 AU it takes 2.98 yr to circle the Sun.

Apollo Observations: 72
Orbital Period · P
2.98 yr
v(q)
52.7 km/s
v(Q)
8.1 km/s
Diameter · ≈
0.07 km
TJ
3.37
Eccentricity · e
0.7334

Orbit and dynamics

The path is an ellipse reaching 0.553 AU from the Sun at perihelion and 3.592 AU at aphelion, a radial span of 3.039 AU.

Applying Kepler's third law to a = 2.072 AU gives an orbital period of 2.98 yr, or about 1,089 days.

The high eccentricity (0.733) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.35° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 52.7 km/s at perihelion and falls to 8.1 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 = 23.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

The current orbit solution is based on 72 observations and has a weighted RMS residual of 0.6796 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
2.072 AU
Eccentricity
0.7334
Perihelion
0.553 AU
Aphelion
3.591605 AU
Inclination
2.35°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
60.21°

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-Oct-20 05:27 0.305244 AU
45663915 km
30.99 km/s
2031-Oct-15 19:06 0.410482 AU
61407204 km
34.21 km/s
2034-Oct-14 21:24 0.441591 AU
66061134 km
34.99 km/s
2037-Oct-11 16:44 0.498503 AU
74574985 km
36.78 km/s
2061-Oct-14 20:14 0.475102 AU
71074182 km
35.66 km/s
2064-Oct-18 16:59 0.394239 AU
58977261 km
33.16 km/s
2067-Oct-22 23:33 0.322472 AU
48241158 km
30.98 km/s
2070-Oct-29 05:43 0.210898 AU
31549836 km
27.40 km/s
2073-Nov-04 17:33 0.082666 AU
12366624 km
23.46 km/s
2076-Nov-11 12:12 0.051730 AU
7738739 km
19.89 km/s
2079-Nov-21 12:02 0.166076 AU
24844597 km
16.30 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
23.4

Orbit Quality

RMS
0.6796
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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