SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 BZ14

2016 BZ14

2016 BZ14 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.862 AU it takes 4.84 yr to circle the Sun.

Apollo Observations: 548
Orbital Period · P
4.84 yr
v(q)
39.3 km/s
v(Q)
7.9 km/s
Diameter · ≈
0.73 km
TJ
2.77
Eccentricity · e
0.6655

Orbit and dynamics

The path is an ellipse reaching 0.957 AU from the Sun at perihelion and 4.767 AU at aphelion, a radial span of 3.81 AU.

Applying Kepler's third law to a = 2.862 AU gives an orbital period of 4.84 yr, or about 1,768 days.

The high eccentricity (0.665) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 31.16° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.3 km/s at perihelion and falls to 7.9 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

The measured diameter is 1.21 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.052 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 548 observations and has a weighted RMS residual of 0.385 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
2.862 AU
Eccentricity
0.6655
Perihelion
0.957 AU
Aphelion
4.766661 AU
Inclination
31.16°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
43.3°

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
2045-Feb-02 21:36 0.068683 AU
10274825 km
22.06 km/s
2069-Feb-10 04:49 0.065660 AU
9822578 km
20.62 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
1.214 km
Albedo
0.052
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
18.44

Orbit Quality

RMS
0.38504
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.

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