SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 RF6

2018 RF6

2018 RF6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.018 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 56
Orbital Period · P
1.03 yr
v(q)
32.1 km/s
v(Q)
27.2 km/s
Diameter · ≈
0.04 km
TJ
5.92
Eccentricity · e
0.0834

Orbit and dynamics

The path is an ellipse reaching 0.933 AU from the Sun at perihelion and 1.103 AU at aphelion, a radial span of 0.17 AU.

Applying Kepler's third law to a = 1.018 AU gives an orbital period of 1.03 yr, or about 375 days.

With e = 0.083, the orbit is close to circular.

A steep inclination of 24.02° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 32.1 km/s at perihelion and falls to 27.2 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 = 25 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 56 observations and has a weighted RMS residual of 0.346 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.018 AU
Eccentricity
0.0834
Perihelion
0.933 AU
Aphelion
1.102901 AU
Inclination
24.02°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
96.17°

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
2054-Sep-04 05:39 0.236409 AU
35366266 km
19.09 km/s
2055-Sep-09 01:45 0.102712 AU
15365570 km
15.78 km/s
2056-Feb-26 23:25 0.260294 AU
38939418 km
17.25 km/s
2056-Sep-12 02:35 0.053672 AU
8029264 km
13.33 km/s
2057-Mar-01 21:17 0.141637 AU
21188641 km
14.45 km/s
2057-Sep-14 22:14 0.032515 AU
4864144 km
12.23 km/s
2058-Mar-07 00:09 0.058911 AU
8812969 km
12.76 km/s
2058-Sep-16 09:14 0.099681 AU
14912128 km
12.71 km/s
2059-Mar-12 20:41 0.004511 AU
674776 km
12.81 km/s
2059-Sep-15 08:16 0.268984 AU
40239388 km
14.55 km/s
2060-Mar-18 21:22 0.128771 AU
19263927 km
14.79 km/s
2061-Mar-26 09:47 0.303326 AU
45376903 km
18.20 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
25.0

Orbit Quality

RMS
0.34597
Condition
7
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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