SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 JN6

2016 JN6

2016 JN6 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.376 AU once every 1.61 yr.

Amor Observations: 38
Orbital Period · P
1.61 yr
v(q)
32.4 km/s
v(Q)
19.9 km/s
Diameter · ≈
0.02 km
TJ
4.78
Eccentricity · e
0.2385

Orbit and dynamics

Between its closest point (1.048 AU) and its farthest (1.704 AU), the heliocentric distance changes by 0.656 AU over every revolution.

One full revolution takes 1.61 yr (590 days), computed from the semi-major axis of 1.376 AU.

An eccentricity of 0.238 makes the orbit moderately elongated.

Its inclination of 1.48° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.4 km/s at perihelion and falls to 19.9 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 25.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 38 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4555 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.376 AU
Eccentricity
0.2385
Perihelion
1.048 AU
Aphelion
1.704176 AU
Inclination
1.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
105.45°

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
2029-Aug-03 04:36 0.459545 AU
68746979 km
5.91 km/s
2037-Mar-24 03:00 0.153414 AU
22950366 km
6.67 km/s
2045-Feb-18 16:07 0.256996 AU
38446116 km
1.27 km/s
2045-May-21 03:54 0.217082 AU
32475040 km
8.86 km/s
2052-Dec-28 14:43 0.476855 AU
71336529 km
6.70 km/s
2058-Mar-10 16:06 0.376672 AU
56349376 km
13.43 km/s
2058-Jul-13 17:23 0.360454 AU
53923131 km
3.91 km/s
2066-Apr-24 22:10 0.052093 AU
7792933 km
2.87 km/s
2074-Jan-12 09:14 0.404175 AU
60463771 km
5.36 km/s
2074-Jun-06 05:41 0.455009 AU
68068308 km
16.11 km/s
2079-Jul-28 09:17 0.419815 AU
62803493 km
5.28 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
25.9

Orbit Quality

RMS
0.45551
Condition
5
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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