SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 AR130

2016 AR130

2016 AR130 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.606 AU it takes 2.04 yr to circle the Sun.

Apollo Observations: 92
Orbital Period · P
2.04 yr
v(q)
53.5 km/s
v(Q)
10.3 km/s
Diameter · ≈
0.29 km
TJ
3.7
Eccentricity · e
0.6762

Orbit and dynamics

Between its closest point (0.52 AU) and its farthest (2.692 AU), the heliocentric distance changes by 2.172 AU over every revolution.

One full revolution takes 2.04 yr (743 days), computed from the semi-major axis of 1.606 AU.

The high eccentricity (0.676) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 55.93° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 53.5 km/s at perihelion and falls to 10.3 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 = 20.44 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.29 km.

Observation record and orbit quality

Astrometry from 92 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3963 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
1.606 AU
Eccentricity
0.6762
Perihelion
0.52 AU
Aphelion
2.691977 AU
Inclination
55.93°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
3.03°

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-Jul-13 13:40 0.314718 AU
47081207 km
38.18 km/s
2030-Jul-26 19:37 0.368043 AU
55058523 km
41.18 km/s
2032-Aug-07 11:07 0.488327 AU
73052703 km
44.86 km/s
2066-Dec-27 18:58 0.408917 AU
61173057 km
41.86 km/s
2069-Jan-03 17:11 0.255433 AU
38212230 km
37.13 km/s
2071-Jan-10 15:00 0.185855 AU
27803532 km
32.97 km/s
2073-Jan-15 03:09 0.280857 AU
42015609 km
29.59 km/s
2075-Jan-18 17:05 0.442337 AU
66172724 km
27.22 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
20.44

Orbit Quality

RMS
0.39631
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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