SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 EC86

2016 EC86

2016 EC86 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.386 AU it takes 1.63 yr to circle the Sun.

Apollo Observations: 72
Orbital Period · P
1.63 yr
v(q)
33.7 km/s
v(Q)
19 km/s
Diameter · ≈
0.18 km
TJ
4.68
Eccentricity · e
0.2791

Orbit and dynamics

Between its closest point (0.999 AU) and its farthest (1.773 AU), the heliocentric distance changes by 0.774 AU over every revolution.

One full revolution takes 1.63 yr (596 days), computed from the semi-major axis of 1.386 AU.

An eccentricity of 0.279 makes the orbit moderately elongated.

A steep inclination of 21.45° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 33.7 km/s at perihelion and falls to 19 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 = 21.49 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.18 km.

Observation record and orbit quality

Astrometry from 72 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6137 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
1.386 AU
Eccentricity
0.2791
Perihelion
0.999 AU
Aphelion
1.772833 AU
Inclination
21.45°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
163.28°

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-13 12:06 0.300621 AU
44972306 km
14.11 km/s
2029-Mar-05 21:05 0.252182 AU
37725884 km
11.19 km/s
2041-Oct-05 10:08 0.291831 AU
43657286 km
11.27 km/s
2042-Mar-02 07:19 0.234972 AU
35151344 km
14.56 km/s
2047-Mar-23 00:49 0.462839 AU
69239709 km
11.06 km/s
2054-Sep-18 08:28 0.467927 AU
70000898 km
11.40 km/s
2059-Oct-14 02:38 0.284092 AU
42499594 km
13.51 km/s
2060-Mar-04 10:31 0.229237 AU
34293308 km
11.33 km/s
2072-Oct-03 18:05 0.307269 AU
45966804 km
11.22 km/s
2073-Mar-02 15:07 0.257961 AU
38590435 km
15.19 km/s
2077-Oct-11 00:07 0.490873 AU
73433496 km
19.63 km/s
2078-Mar-20 13:25 0.439964 AU
65817729 km
11.05 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
21.49

Orbit Quality

RMS
0.61365
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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