SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 BK5

2020 BK5

2020 BK5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.224 AU it takes 1.35 yr to circle the Sun.

Apollo Observations: 43
Orbital Period · P
1.35 yr
v(q)
43.1 km/s
v(Q)
16.8 km/s
Diameter · ≈
0.09 km
TJ
5.08
Eccentricity · e
0.4399

Orbit and dynamics

The path is an ellipse reaching 0.686 AU from the Sun at perihelion and 1.762 AU at aphelion, a radial span of 1.076 AU.

Applying Kepler's third law to a = 1.224 AU gives an orbital period of 1.35 yr, or about 495 days.

The high eccentricity (0.44) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 18.77° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43.1 km/s at perihelion and falls to 16.8 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 = 22.97 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 43 observations and has a weighted RMS residual of 0.4746 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
1.224 AU
Eccentricity
0.4399
Perihelion
0.686 AU
Aphelion
1.762438 AU
Inclination
18.77°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
175.76°

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
2028-Jul-30 03:37 0.226411 AU
33870568 km
14.87 km/s
2032-Sep-05 20:22 0.212846 AU
31841340 km
20.36 km/s
2035-Feb-07 16:17 0.406235 AU
60771853 km
27.66 km/s
2039-Feb-20 20:16 0.172390 AU
25789134 km
16.80 km/s
2043-Feb-12 08:13 0.319324 AU
47770169 km
11.97 km/s
2055-Sep-15 16:26 0.265257 AU
39681911 km
24.07 km/s
2058-Feb-12 22:32 0.237432 AU
35519329 km
23.58 km/s
2062-Feb-22 04:57 0.174668 AU
26129982 km
13.79 km/s
2066-Feb-04 12:48 0.378830 AU
56672115 km
12.36 km/s
2078-Sep-21 04:05 0.318122 AU
47590397 km
26.77 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
22.97

Orbit Quality

RMS
0.47461
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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