SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 BR80

2016 BR80

2016 BR80 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.703 AU it takes 2.22 yr to circle the Sun.

Apollo Observations: 55
Orbital Period · P
2.22 yr
v(q)
37.2 km/s
v(Q)
14 km/s
Diameter · ≈
0.2 km
TJ
4.05
Eccentricity · e
0.4527

Orbit and dynamics

The path is an ellipse reaching 0.932 AU from the Sun at perihelion and 2.474 AU at aphelion, a radial span of 1.542 AU.

Applying Kepler's third law to a = 1.703 AU gives an orbital period of 2.22 yr, or about 812 days.

The high eccentricity (0.453) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 12.08° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37.2 km/s at perihelion and falls to 14 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 0.21 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.123 points to a comparatively bright, reflective surface.

Observation record and orbit quality

The current orbit solution is based on 55 observations and has a weighted RMS residual of 0.526 arcseconds.

Condition code U = 1 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
1.703 AU
Eccentricity
0.4527
Perihelion
0.932 AU
Aphelion
2.473948 AU
Inclination
12.08°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
224.19°

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-May-17 10:12 0.401608 AU
60079630 km
20.52 km/s
2036-Feb-14 07:40 0.161253 AU
24123069 km
10.80 km/s
2047-May-15 23:33 0.378568 AU
56632986 km
19.80 km/s
2056-Feb-07 22:49 0.182910 AU
27363010 km
11.46 km/s
2067-May-11 13:54 0.313245 AU
46860791 km
17.93 km/s
2076-Jan-27 19:16 0.238147 AU
35626350 km
13.45 km/s

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

Physical Parameters

Diameter
0.208 km
Albedo
0.123
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
21.3

Orbit Quality

RMS
0.52596
Condition
1
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.