SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 FU

2018 FU

2018 FU belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.263 AU it takes 1.42 yr to circle the Sun.

Apollo Observations: 106
Orbital Period · P
1.42 yr
v(q)
44.7 km/s
v(Q)
15.7 km/s
Diameter · ≈
0.13 km
TJ
4.97
Eccentricity · e
0.4791

Orbit and dynamics

The path is an ellipse reaching 0.658 AU from the Sun at perihelion and 1.868 AU at aphelion, a radial span of 1.21 AU.

Applying Kepler's third law to a = 1.263 AU gives an orbital period of 1.42 yr, or about 518 days.

The high eccentricity (0.479) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.07° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.7 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 = 22.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

The current orbit solution is based on 106 observations and has a weighted RMS residual of 0.4412 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
1.263 AU
Eccentricity
0.4791
Perihelion
0.658 AU
Aphelion
1.868103 AU
Inclination
9.07°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
336.64°

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-Dec-23 16:11 0.334775 AU
50081630 km
13.79 km/s
2028-Mar-25 02:53 0.429067 AU
64187492 km
9.36 km/s
2030-Aug-21 22:45 0.208755 AU
31229302 km
21.17 km/s
2035-Mar-15 03:32 0.125330 AU
18749069 km
19.27 km/s
2037-Oct-30 08:31 0.280208 AU
41918523 km
13.10 km/s
2047-Sep-03 19:08 0.079329 AU
11867469 km
14.95 km/s
2052-Mar-24 14:25 0.259182 AU
38773064 km
25.78 km/s
2057-Aug-13 04:26 0.231758 AU
34670488 km
26.15 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
22.2

Orbit Quality

RMS
0.44123
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.

Keep exploring

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