SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 MQ130

2015 MQ130

2015 MQ130 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.206 AU once every 3.28 yr.

Amor Observations: 59
Orbital Period · P
3.28 yr
v(q)
36.4 km/s
v(Q)
11.1 km/s
Diameter · ≈
0.23 km
TJ
3.2
Eccentricity · e
0.5338

Orbit and dynamics

Between its closest point (1.028 AU) and its farthest (3.384 AU), the heliocentric distance changes by 2.356 AU over every revolution.

One full revolution takes 3.28 yr (1,197 days), computed from the semi-major axis of 2.206 AU.

The high eccentricity (0.534) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 40.2° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36.4 km/s at perihelion and falls to 11.1 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

The measured diameter is 0.36 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.012 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 59 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3995 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
2.206 AU
Eccentricity
0.5338
Perihelion
1.028 AU
Aphelion
3.383563 AU
Inclination
40.2°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
107.82°

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
2028-Nov-13 20:06 0.281723 AU
42145200 km
24.50 km/s
2051-Nov-08 00:34 0.433873 AU
64906519 km
20.45 km/s
2064-Nov-18 23:54 0.397604 AU
59480760 km
27.80 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.36 km
Albedo
0.012
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.9

Orbit Quality

RMS
0.39947
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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