SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 BF14

2020 BF14

2020 BF14 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.284 AU it takes 1.45 yr to circle the Sun.

Apollo Observations: 48
Orbital Period · P
1.45 yr
v(q)
44.1 km/s
v(Q)
15.7 km/s
Diameter · ≈
0.63 km
TJ
4.76
Eccentricity · e
0.4751

Orbit and dynamics

The path is an ellipse reaching 0.674 AU from the Sun at perihelion and 1.894 AU at aphelion, a radial span of 1.22 AU.

Applying Kepler's third law to a = 1.284 AU gives an orbital period of 1.45 yr, or about 531 days.

The high eccentricity (0.475) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 36.14° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 44.1 km/s at perihelion and falls to 15.7 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 = 18.76 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.63 km.

Observation record and orbit quality

The current orbit solution is based on 48 observations and has a weighted RMS residual of 0.4399 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
1.284 AU
Eccentricity
0.4751
Perihelion
0.674 AU
Aphelion
1.894028 AU
Inclination
36.14°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
187.61°

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
2030-Mar-13 11:42 0.155954 AU
23330424 km
25.90 km/s
2033-Feb-27 10:58 0.393956 AU
58934997 km
18.10 km/s
2035-Sep-19 17:28 0.195758 AU
29284955 km
20.38 km/s
2038-Aug-23 21:28 0.348560 AU
52143802 km
30.53 km/s
2046-Mar-15 13:33 0.206764 AU
30931520 km
27.08 km/s
2049-Feb-27 15:05 0.340605 AU
50953784 km
18.41 km/s
2051-Sep-22 18:49 0.251573 AU
37634778 km
19.74 km/s
2054-Aug-26 17:45 0.292108 AU
43698799 km
29.18 km/s
2062-Mar-18 04:25 0.268824 AU
40215424 km
28.55 km/s
2065-Feb-28 10:06 0.276941 AU
41429850 km
18.94 km/s
2067-Sep-26 09:37 0.316039 AU
47278702 km
19.18 km/s
2070-Aug-29 20:20 0.230831 AU
34531814 km
27.76 km/s
2078-Mar-20 19:03 0.329644 AU
49314030 km
30.05 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
18.76

Orbit Quality

RMS
0.43988
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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