SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 MR8

2018 MR8

2018 MR8 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.972 AU and a period of 0.96 yr.

Aten Observations: 239
Orbital Period · P
0.96 yr
v(q)
36.2 km/s
v(Q)
25.2 km/s
Diameter · ≈
0.3 km
TJ
6.1
Eccentricity · e
0.1782

Orbit and dynamics

Between its closest point (0.799 AU) and its farthest (1.146 AU), the heliocentric distance changes by 0.347 AU over every revolution.

One full revolution takes 0.96 yr (350 days), computed from the semi-major axis of 0.972 AU.

An eccentricity of 0.178 makes the orbit moderately elongated.

A steep inclination of 27.95° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36.2 km/s at perihelion and falls to 25.2 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 = 20.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.3 km.

Observation record and orbit quality

Astrometry from 239 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3989 arcseconds.

Condition code U = 1 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
0.9723 AU
Eccentricity
0.1782
Perihelion
0.799 AU
Aphelion
1.145564 AU
Inclination
27.95°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
310.48°

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
2039-Feb-10 14:46 0.342843 AU
51288538 km
19.22 km/s
2039-Jun-26 16:54 0.411343 AU
61535966 km
15.65 km/s
2040-Jan-19 09:32 0.186799 AU
27944662 km
17.15 km/s
2040-Jul-05 17:02 0.231471 AU
34627637 km
14.05 km/s
2040-Dec-26 06:11 0.226396 AU
33868426 km
16.87 km/s
2041-Jul-12 15:14 0.105219 AU
15740587 km
13.91 km/s
2041-Nov-29 01:11 0.395771 AU
59206500 km
17.44 km/s
2042-Jul-15 20:55 0.232812 AU
34828184 km
16.03 km/s
2043-Jul-14 20:05 0.440691 AU
65926373 km
20.30 km/s
2062-Feb-16 09:49 0.394713 AU
59048286 km
20.02 km/s
2062-Jun-23 12:28 0.458303 AU
68561085 km
16.21 km/s
2063-Jan-25 02:17 0.216438 AU
32378629 km
17.52 km/s
2063-Jul-04 06:43 0.277413 AU
41500441 km
14.35 km/s
2064-Jan-02 08:51 0.194326 AU
29070710 km
16.78 km/s
2064-Jul-11 01:23 0.119742 AU
17913148 km
13.76 km/s
2064-Dec-06 19:09 0.349542 AU
52290776 km
17.38 km/s
2065-Jul-15 07:07 0.184962 AU
27669967 km
15.24 km/s
2066-Jul-15 09:23 0.385526 AU
57673865 km
19.05 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
20.4

Orbit Quality

RMS
0.39893
Condition
1
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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