SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 MA6

2014 MA6

2014 MA6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.265 AU it takes 1.42 yr to circle the Sun.

Apollo Observations: 95
Orbital Period · P
1.42 yr
v(q)
32.8 km/s
v(Q)
21.3 km/s
Diameter · ≈
0.05 km
TJ
5.08
Eccentricity · e
0.2123

Orbit and dynamics

Between its closest point (0.997 AU) and its farthest (1.534 AU), the heliocentric distance changes by 0.537 AU over every revolution.

One full revolution takes 1.42 yr (520 days), computed from the semi-major axis of 1.265 AU.

An eccentricity of 0.212 makes the orbit moderately elongated.

Its inclination of 3.18° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.8 km/s at perihelion and falls to 21.3 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 = 24.39 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 95 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3924 arcseconds.

Condition code U = 5 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
1.265 AU
Eccentricity
0.2123
Perihelion
0.997 AU
Aphelion
1.533559 AU
Inclination
3.18°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
105.14°

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
2031-Apr-20 06:44 0.400398 AU
59898660 km
6.16 km/s
2031-Oct-21 12:30 0.401345 AU
60040371 km
16.13 km/s
2034-Jun-12 12:58 0.428592 AU
64116405 km
16.86 km/s
2034-Dec-20 08:06 0.411900 AU
61619323 km
6.67 km/s
2041-May-21 09:40 0.279269 AU
41778099 km
3.61 km/s
2041-Oct-08 16:39 0.161242 AU
24121403 km
8.98 km/s
2045-Jan-07 18:53 0.480916 AU
71944069 km
7.83 km/s
2051-Aug-29 03:52 0.056512 AU
8454039 km
3.46 km/s
2058-Mar-25 00:41 0.492634 AU
73696940 km
7.82 km/s
2061-Jun-30 18:52 0.107356 AU
16060156 km
7.49 km/s
2061-Nov-07 04:55 0.243658 AU
36450713 km
3.07 km/s
2068-Apr-12 03:47 0.428264 AU
64067309 km
6.68 km/s
2068-Oct-24 18:15 0.476437 AU
71273902 km
18.46 km/s
2071-Jun-16 18:15 0.350134 AU
52379233 km
14.66 km/s
2071-Dec-13 11:43 0.380637 AU
56942470 km
6.11 km/s
2078-May-10 18:55 0.319387 AU
47779581 km
4.55 km/s
2078-Oct-13 00:21 0.226738 AU
33919552 km
10.97 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
24.39

Orbit Quality

RMS
0.39238
Condition
5
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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