SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 RO5

2018 RO5

2018 RO5 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.992 AU and a period of 0.99 yr.

Aten Observations: 102
Orbital Period · P
0.99 yr
v(q)
37.9 km/s
v(Q)
23.6 km/s
Diameter · ≈
0.03 km
TJ
6.1
Eccentricity · e
0.2317

Orbit and dynamics

Between its closest point (0.762 AU) and its farthest (1.221 AU), the heliocentric distance changes by 0.459 AU over every revolution.

One full revolution takes 0.99 yr (361 days), computed from the semi-major axis of 0.992 AU.

An eccentricity of 0.232 makes the orbit moderately elongated.

Its inclination of 2.68° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.9 km/s at perihelion and falls to 23.6 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 = 25.61 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 102 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5368 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
0.9916 AU
Eccentricity
0.2317
Perihelion
0.762 AU
Aphelion
1.221354 AU
Inclination
2.68°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
25.28°

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
2026-Dec-21 06:18 0.211574 AU
31650976 km
6.03 km/s
2027-Apr-15 17:29 0.218858 AU
32740654 km
7.22 km/s
2028-Jan-05 16:16 0.178701 AU
26733247 km
5.39 km/s
2028-Mar-27 17:11 0.185490 AU
27748912 km
5.92 km/s
2029-Jan-27 08:31 0.124174 AU
18576224 km
4.40 km/s
2030-Feb-08 22:02 0.051485 AU
7702109 km
5.77 km/s
2031-Feb-07 05:36 0.023649 AU
3537790 km
7.90 km/s
2032-Feb-04 08:51 0.090690 AU
13567062 km
10.40 km/s
2033-Jan-31 03:43 0.175366 AU
26234413 km
13.02 km/s
2034-Jan-27 16:11 0.263201 AU
39374281 km
15.72 km/s
2035-Jan-24 03:23 0.351325 AU
52557406 km
18.46 km/s
2036-Jan-20 15:41 0.438978 AU
65670162 km
21.20 km/s
2079-Sep-29 00:42 0.446246 AU
66757411 km
21.15 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
25.61

Orbit Quality

RMS
0.53679
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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