SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 MC5

2018 MC5

2018 MC5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.373 AU it takes 1.61 yr to circle the Sun.

Apollo Observations: 54
Orbital Period · P
1.61 yr
v(q)
33.4 km/s
v(Q)
19.4 km/s
Diameter · ≈
0.03 km
TJ
4.78
Eccentricity · e
0.2651

Orbit and dynamics

The path is an ellipse reaching 1.009 AU from the Sun at perihelion and 1.737 AU at aphelion, a radial span of 0.728 AU.

Applying Kepler's third law to a = 1.373 AU gives an orbital period of 1.61 yr, or about 588 days.

An eccentricity of 0.265 makes the orbit moderately elongated.

Its inclination of 1.03° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.4 km/s at perihelion and falls to 19.4 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 25.33 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 54 observations and has a weighted RMS residual of 0.5499 arcseconds.

Condition code U = 5 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
1.373 AU
Eccentricity
0.2651
Perihelion
1.009 AU
Aphelion
1.736982 AU
Inclination
1.03°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
315.21°

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
2034-Apr-20 20:18 0.478441 AU
71573760 km
6.48 km/s
2034-Oct-09 15:33 0.456920 AU
68354263 km
18.25 km/s
2039-Jun-05 14:12 0.455922 AU
68204961 km
18.20 km/s
2039-Nov-26 17:00 0.480105 AU
71822698 km
6.76 km/s
2047-Jun-26 04:42 0.122778 AU
18367299 km
8.42 km/s
2055-Sep-11 14:03 0.048171 AU
7206317 km
5.95 km/s
2063-Apr-20 17:00 0.482327 AU
72155057 km
6.58 km/s
2063-Oct-11 00:30 0.464124 AU
69431975 km
18.66 km/s
2068-Jun-08 21:52 0.369650 AU
55298904 km
16.24 km/s
2068-Nov-20 07:10 0.438337 AU
65574344 km
6.13 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
25.33

Orbit Quality

RMS
0.54987
Condition
5
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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