SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 MQ3

2012 MQ3

2012 MQ3 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.366 AU once every 1.60 yr.

Amor Observations: 100
Orbital Period · P
1.60 yr
v(q)
30.5 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.12 km
TJ
4.81
Eccentricity · e
0.1783

Orbit and dynamics

Between its closest point (1.123 AU) and its farthest (1.61 AU), the heliocentric distance changes by 0.487 AU over every revolution.

One full revolution takes 1.60 yr (583 days), computed from the semi-major axis of 1.366 AU.

An eccentricity of 0.178 makes the orbit moderately elongated.

The orbital plane is tilted 7.95° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 30.5 km/s at perihelion and falls to 21.3 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

No direct size measurement is available; from an absolute magnitude of H = 22.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

Astrometry from 100 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4882 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
1.366 AU
Eccentricity
0.1783
Perihelion
1.123 AU
Aphelion
1.609558 AU
Inclination
7.95°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
252.95°

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-Sep-25 04:29 0.318263 AU
47611477 km
2.25 km/s
2036-Oct-14 01:41 0.365628 AU
54697227 km
4.19 km/s
2039-Mar-28 12:27 0.498792 AU
74618178 km
6.25 km/s
2044-Oct-27 06:31 0.407169 AU
60911613 km
5.49 km/s
2047-Apr-08 11:12 0.460692 AU
68918518 km
5.47 km/s
2052-Nov-07 01:13 0.444017 AU
66423986 km
6.43 km/s
2055-Apr-21 11:48 0.414690 AU
62036744 km
4.67 km/s
2060-Nov-16 14:28 0.477914 AU
71494905 km
7.22 km/s
2063-May-07 18:42 0.358420 AU
53618837 km
3.95 km/s
2071-May-28 02:55 0.291430 AU
43597346 km
3.81 km/s
2079-Jun-16 02:17 0.224726 AU
33618579 km
4.11 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
22.3

Orbit Quality

RMS
0.48818
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.

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