SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 EQ85

2016 EQ85

2016 EQ85 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.054 AU it takes 1.08 yr to circle the Sun.

Apollo Observations: 20
Orbital Period · P
1.08 yr
v(q)
35.6 km/s
v(Q)
23.6 km/s
Diameter · ≈
0.01 km
TJ
5.81
Eccentricity · e
0.203

Orbit and dynamics

Between its closest point (0.84 AU) and its farthest (1.268 AU), the heliocentric distance changes by 0.428 AU over every revolution.

One full revolution takes 1.08 yr (395 days), computed from the semi-major axis of 1.054 AU.

An eccentricity of 0.203 makes the orbit moderately elongated.

The orbital plane is tilted 7.33° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.6 km/s at perihelion and falls to 23.6 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 = 27.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 20 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6471 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
1.054 AU
Eccentricity
0.203
Perihelion
0.84 AU
Aphelion
1.267962 AU
Inclination
7.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
244.89°

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-Sep-03 08:35 0.017581 AU
2630085 km
7.74 km/s
2029-Mar-01 03:58 0.034955 AU
5229123 km
4.78 km/s
2030-Mar-15 22:05 0.346435 AU
51825893 km
18.20 km/s
2040-Aug-20 03:38 0.121374 AU
18157249 km
14.31 km/s
2043-Mar-05 08:27 0.022602 AU
3381144 km
11.00 km/s
2057-Mar-15 04:19 0.206319 AU
30864829 km
17.34 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
27.6

Orbit Quality

RMS
0.64711
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.