SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 EV84

2016 EV84

2016 EV84 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.866 AU and a period of 0.81 yr.

Aten Observations: 103
Orbital Period · P
0.81 yr
v(q)
38.3 km/s
v(Q)
26.7 km/s
Diameter · ≈
0.02 km
TJ
6.79
Eccentricity · e
0.1779

Orbit and dynamics

The path is an ellipse reaching 0.712 AU from the Sun at perihelion and 1.02 AU at aphelion, a radial span of 0.308 AU.

Applying Kepler's third law to a = 0.866 AU gives an orbital period of 0.81 yr, or about 294 days.

An eccentricity of 0.178 makes the orbit moderately elongated.

The orbital plane is tilted 13.58° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 38.3 km/s at perihelion and falls to 26.7 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 = 26.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 103 observations and has a weighted RMS residual of 0.4366 arcseconds.

Condition code U = 6 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
0.8662 AU
Eccentricity
0.1779
Perihelion
0.712 AU
Aphelion
1.020297 AU
Inclination
13.58°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
52.39°

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-Sep-20 05:37 0.291013 AU
43534989 km
11.64 km/s
2032-Oct-16 05:36 0.299590 AU
44818044 km
10.98 km/s
2033-Apr-08 03:22 0.367163 AU
54926812 km
14.63 km/s
2036-Nov-13 17:01 0.302773 AU
45294233 km
8.59 km/s
2037-Apr-02 13:47 0.227154 AU
33981785 km
10.28 km/s
2041-Mar-24 22:06 0.096028 AU
14365656 km
8.20 km/s
2045-Mar-15 06:07 0.024789 AU
3708450 km
7.39 km/s
2049-Mar-09 12:38 0.015692 AU
2347551 km
7.64 km/s
2053-Mar-04 17:34 0.118724 AU
17760837 km
9.34 km/s
2053-Jul-21 10:23 0.279774 AU
41853637 km
8.46 km/s
2057-Mar-04 03:02 0.192575 AU
28808882 km
12.58 km/s
2061-Mar-06 18:22 0.251282 AU
37591264 km
16.35 km/s
2070-Apr-07 10:33 0.212701 AU
31819613 km
16.31 km/s
2074-Apr-06 07:27 0.124165 AU
18574799 km
12.42 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
26.7

Orbit Quality

RMS
0.43662
Condition
6
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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