SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 AU192

2016 AU192

2016 AU192 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.135 AU it takes 1.21 yr to circle the Sun.

Apollo Observations: 18
Orbital Period · P
1.21 yr
v(q)
41.9 km/s
v(Q)
18.6 km/s
Diameter · ≈
0.15 km
TJ
5.37
Eccentricity · e
0.3847

Orbit and dynamics

The path is an ellipse reaching 0.699 AU from the Sun at perihelion and 1.572 AU at aphelion, a radial span of 0.873 AU.

Applying Kepler's third law to a = 1.135 AU gives an orbital period of 1.21 yr, or about 442 days.

An eccentricity of 0.385 makes the orbit moderately elongated.

A steep inclination of 24.05° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 41.9 km/s at perihelion and falls to 18.6 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 = 21.9 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 18 observations and has a weighted RMS residual of 0.2942 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
1.135 AU
Eccentricity
0.3847
Perihelion
0.699 AU
Aphelion
1.571635 AU
Inclination
24.05°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
92.87°

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-10 07:14 0.345780 AU
51727892 km
15.32 km/s
2028-Aug-26 10:37 0.364456 AU
54521846 km
19.04 km/s
2033-Jan-27 02:24 0.390057 AU
58351734 km
13.81 km/s
2033-May-07 18:35 0.401074 AU
59999827 km
16.86 km/s
2039-Jan-12 01:39 0.483622 AU
72348883 km
14.50 km/s
2039-Jun-15 10:01 0.329483 AU
49289940 km
18.85 km/s
2045-Jul-18 13:28 0.290492 AU
43457027 km
18.35 km/s
2050-Feb-10 23:16 0.353251 AU
52845558 km
16.13 km/s
2051-Aug-22 11:17 0.346881 AU
51892687 km
18.63 km/s
2056-Jan-30 04:50 0.378940 AU
56688635 km
13.75 km/s
2056-May-01 09:57 0.408288 AU
61079009 km
16.12 km/s
2062-Jan-14 04:27 0.469743 AU
70272483 km
14.41 km/s
2062-Jun-09 21:52 0.340086 AU
50876168 km
18.79 km/s
2068-Jul-13 02:49 0.291745 AU
43644369 km
18.48 km/s
2073-Feb-10 23:40 0.365872 AU
54733670 km
17.13 km/s
2074-Aug-16 08:40 0.329098 AU
49232390 km
18.31 km/s
2079-Feb-03 02:30 0.360037 AU
53860753 km
13.82 km/s
2079-Apr-17 17:01 0.417471 AU
62452807 km
13.82 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
21.9

Orbit Quality

RMS
0.2942
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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