SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 ED195

2016 ED195

2016 ED195 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.968 AU it takes 2.76 yr to circle the Sun.

Apollo Observations: 170
Orbital Period · P
2.76 yr
v(q)
42.3 km/s
v(Q)
10.7 km/s
Diameter · ≈
0.61 km
TJ
3.44
Eccentricity · e
0.5968

Orbit and dynamics

Between its closest point (0.793 AU) and its farthest (3.143 AU), the heliocentric distance changes by 2.35 AU over every revolution.

One full revolution takes 2.76 yr (1,008 days), computed from the semi-major axis of 1.968 AU.

The high eccentricity (0.597) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 36.6° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 42.3 km/s at perihelion and falls to 10.7 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 = 18.84 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.61 km.

Observation record and orbit quality

Astrometry from 170 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3797 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
1.968 AU
Eccentricity
0.5968
Perihelion
0.793 AU
Aphelion
3.142502 AU
Inclination
36.6°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
219.88°

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-Apr-21 17:36 0.487018 AU
72856817 km
20.55 km/s
2038-Aug-15 19:54 0.476498 AU
71283035 km
21.48 km/s
2049-Sep-06 09:01 0.270161 AU
40415475 km
21.93 km/s
2060-Sep-21 19:50 0.059542 AU
8907312 km
24.55 km/s
2071-Oct-04 16:20 0.195720 AU
29279359 km
28.46 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
18.84

Orbit Quality

RMS
0.3797
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.

Keep exploring

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