SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 MR5

2018 MR5

2018 MR5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.075 AU it takes 2.99 yr to circle the Sun.

Apollo Observations: 75
Orbital Period · P
2.99 yr
v(q)
50.9 km/s
v(Q)
8.4 km/s
Diameter · ≈
0.22 km
TJ
3.39
Eccentricity · e
0.7169

Orbit and dynamics

The path is an ellipse reaching 0.587 AU from the Sun at perihelion and 3.563 AU at aphelion, a radial span of 2.976 AU.

Applying Kepler's third law to a = 2.075 AU gives an orbital period of 2.99 yr, or about 1,092 days.

The high eccentricity (0.717) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.76° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 50.9 km/s at perihelion and falls to 8.4 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 = 21.08 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

The current orbit solution is based on 75 observations and has a weighted RMS residual of 0.4573 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
2.075 AU
Eccentricity
0.7169
Perihelion
0.587 AU
Aphelion
3.562568 AU
Inclination
2.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
263.77°

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-Apr-10 20:59 0.380978 AU
56993571 km
18.93 km/s
2030-Apr-03 00:02 0.393668 AU
58891885 km
19.84 km/s
2033-Mar-25 02:13 0.402736 AU
60248419 km
20.59 km/s
2036-Mar-25 09:39 0.394545 AU
59023116 km
20.18 km/s
2039-Mar-24 12:52 0.396945 AU
59382121 km
20.34 km/s
2042-Mar-23 08:15 0.397095 AU
59404616 km
20.37 km/s
2045-Mar-20 18:43 0.397973 AU
59535940 km
20.47 km/s
2048-Mar-26 01:24 0.386810 AU
57865980 km
19.83 km/s
2051-Mar-31 21:17 0.382817 AU
57268536 km
19.48 km/s
2054-Apr-06 08:21 0.374191 AU
55978122 km
18.85 km/s
2057-Apr-10 07:13 0.366482 AU
54824957 km
18.35 km/s
2060-Apr-23 16:31 0.326175 AU
48795100 km
16.23 km/s
2063-May-14 08:23 0.259449 AU
38812974 km
14.30 km/s
2066-May-30 13:50 0.158447 AU
23703349 km
16.07 km/s
2069-Jun-07 04:55 0.072259 AU
10809798 km
18.79 km/s
2072-Jun-14 11:13 0.083325 AU
12465284 km
22.48 km/s
2075-Jun-23 01:59 0.218954 AU
32755065 km
26.71 km/s
2078-Jun-30 08:41 0.366118 AU
54770407 km
31.06 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
21.08

Orbit Quality

RMS
0.45727
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.

Keep exploring

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