SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 MQ3

2011 MQ3

2011 MQ3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.122 AU it takes 1.19 yr to circle the Sun.

Apollo Observations: 72
Orbital Period · P
1.19 yr
v(q)
31.4 km/s
v(Q)
25.2 km/s
Diameter · ≈
0.04 km
TJ
5.56
Eccentricity · e
0.11

Orbit and dynamics

Between its closest point (0.999 AU) and its farthest (1.245 AU), the heliocentric distance changes by 0.246 AU over every revolution.

One full revolution takes 1.19 yr (434 days), computed from the semi-major axis of 1.122 AU.

An eccentricity of 0.11 makes the orbit moderately elongated.

The orbital plane is tilted 5.68° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 31.4 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 = 24.8 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 72 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4142 arcseconds.

Condition code U = 6 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
1.122 AU
Eccentricity
0.11
Perihelion
0.999 AU
Aphelion
1.24542 AU
Inclination
5.68°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
254.91°

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
2030-Jan-03 14:50 0.177089 AU
26492161 km
4.48 km/s
2030-Jun-27 11:26 0.136486 AU
20418069 km
7.96 km/s
2036-Mar-19 12:51 0.105353 AU
15760544 km
4.48 km/s
2042-Feb-28 00:50 0.428386 AU
64085563 km
15.56 km/s
2042-Oct-20 07:05 0.266140 AU
39813982 km
4.85 km/s
2048-Dec-15 03:50 0.220028 AU
32915781 km
4.97 km/s
2049-Jul-03 00:44 0.271781 AU
40657886 km
11.07 km/s
2055-Jun-04 02:53 0.075381 AU
11276768 km
3.10 km/s
2061-Feb-27 21:39 0.438937 AU
65664026 km
15.34 km/s
2061-Oct-19 18:56 0.265099 AU
39658179 km
4.81 km/s
2067-Dec-26 17:47 0.194243 AU
29058363 km
4.70 km/s
2068-Jun-29 09:16 0.189535 AU
28354093 km
9.14 km/s
2074-Mar-14 09:49 0.135879 AU
20327222 km
6.19 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
24.8

Orbit Quality

RMS
0.41422
Condition
6
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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