SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 RU1

2016 RU1

2016 RU1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.204 AU it takes 3.27 yr to circle the Sun.

Apollo Observations: 44
Orbital Period · P
3.27 yr
v(q)
38.1 km/s
v(Q)
10.6 km/s
Diameter · ≈
0.01 km
TJ
3.43
Eccentricity · e
0.5657

Orbit and dynamics

The path is an ellipse reaching 0.957 AU from the Sun at perihelion and 3.451 AU at aphelion, a radial span of 2.494 AU.

Applying Kepler's third law to a = 2.204 AU gives an orbital period of 3.27 yr, or about 1,195 days.

The high eccentricity (0.566) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 0.58° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.1 km/s at perihelion and falls to 10.6 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

The current orbit solution is based on 44 observations and has a weighted RMS residual of 0.4821 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
2.204 AU
Eccentricity
0.5657
Perihelion
0.957 AU
Aphelion
3.450803 AU
Inclination
0.58°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
1.3°

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
2052-Sep-06 03:48 0.010390 AU
1554248 km
10.56 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
0.48206
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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