SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 ET1

2016 ET1

2016 ET1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.08 AU it takes 1.12 yr to circle the Sun.

Apollo Observations: 41
Orbital Period · P
1.12 yr
v(q)
33.8 km/s
v(Q)
24.3 km/s
Diameter · ≈
0.01 km
TJ
5.71
Eccentricity · e
0.1652

Orbit and dynamics

The path is an ellipse reaching 0.902 AU from the Sun at perihelion and 1.258 AU at aphelion, a radial span of 0.356 AU.

Applying Kepler's third law to a = 1.08 AU gives an orbital period of 1.12 yr, or about 410 days.

An eccentricity of 0.165 makes the orbit moderately elongated.

The orbital plane is tilted 6.4° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.8 km/s at perihelion and falls to 24.3 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 = 28.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 41 observations and has a weighted RMS residual of 0.3916 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
1.08 AU
Eccentricity
0.1652
Perihelion
0.902 AU
Aphelion
1.258416 AU
Inclination
6.4°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
105.69°

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
2033-Sep-12 13:06 0.117062 AU
17512282 km
3.95 km/s
2033-Dec-01 18:22 0.129924 AU
19436402 km
3.46 km/s
2034-Apr-06 02:03 0.180925 AU
27065932 km
3.64 km/s
2042-Sep-28 08:29 0.053591 AU
8017051 km
5.39 km/s
2043-May-11 21:52 0.244274 AU
36542822 km
4.50 km/s
2044-Mar-23 10:50 0.442897 AU
66256495 km
17.81 km/s
2051-Sep-24 00:24 0.173471 AU
25950934 km
9.98 km/s
2052-Jun-13 05:44 0.269791 AU
40360198 km
5.05 km/s
2053-Mar-15 05:08 0.256333 AU
38346858 km
12.72 km/s
2060-Sep-15 11:55 0.345391 AU
51669749 km
15.26 km/s
2061-Jul-15 12:27 0.245297 AU
36695970 km
5.09 km/s
2062-Mar-05 17:39 0.061055 AU
9133664 km
7.49 km/s
2069-Sep-10 11:56 0.482993 AU
72254737 km
18.93 km/s
2070-Aug-07 14:39 0.209326 AU
31314748 km
4.77 km/s
2071-Feb-24 22:49 0.029373 AU
4394120 km
4.58 km/s
2079-Sep-27 04:26 0.051959 AU
7773029 km
4.63 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
28.9

Orbit Quality

RMS
0.39164
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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