SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 EQ84

2016 EQ84

2016 EQ84 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.392 AU it takes 1.64 yr to circle the Sun.

Apollo Observations: 29
Orbital Period · P
1.64 yr
v(q)
44.8 km/s
v(Q)
14.2 km/s
Diameter · ≈
0.05 km
TJ
4.62
Eccentricity · e
0.5188

Orbit and dynamics

Between its closest point (0.67 AU) and its farthest (2.114 AU), the heliocentric distance changes by 1.444 AU over every revolution.

One full revolution takes 1.64 yr (600 days), computed from the semi-major axis of 1.392 AU.

The high eccentricity (0.519) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.35° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.8 km/s at perihelion and falls to 14.2 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 = 24.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 29 individual observations underpins this orbit; the fit leaves an RMS residual of 0.885 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.392 AU
Eccentricity
0.5188
Perihelion
0.67 AU
Aphelion
2.11417 AU
Inclination
6.35°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
44.19°

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
2039-Mar-28 21:58 0.023335 AU
3490884 km
15.33 km/s
2044-Mar-07 22:18 0.271406 AU
40601742 km
27.16 km/s
2047-Oct-03 16:39 0.074680 AU
11171983 km
20.70 km/s
2057-Jun-27 12:44 0.356686 AU
53359418 km
15.54 km/s
2062-Apr-29 12:10 0.230990 AU
34555664 km
11.36 km/s
2067-Mar-20 12:40 0.126136 AU
18869657 km
19.90 km/s
2070-Oct-14 18:22 0.378172 AU
56573784 km
27.79 km/s
2075-Sep-25 08:44 0.030038 AU
4493564 km
15.76 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
24.1

Orbit Quality

RMS
0.88495
Condition
7
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.

Keep exploring

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