SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 RN6

2012 RN6

2012 RN6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.644 AU it takes 2.11 yr to circle the Sun.

Apollo Observations: 93
Orbital Period · P
2.11 yr
v(q)
50.6 km/s
v(Q)
10.7 km/s
Diameter · ≈
0.21 km
TJ
4.02
Eccentricity · e
0.6514

Orbit and dynamics

Between its closest point (0.573 AU) and its farthest (2.715 AU), the heliocentric distance changes by 2.142 AU over every revolution.

One full revolution takes 2.11 yr (770 days), computed from the semi-major axis of 1.644 AU.

The high eccentricity (0.651) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.24° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 50.6 km/s at perihelion and falls to 10.7 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 = 21.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.21 km.

Observation record and orbit quality

Astrometry from 93 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4339 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
1.644 AU
Eccentricity
0.6514
Perihelion
0.573 AU
Aphelion
2.714902 AU
Inclination
3.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
216.14°

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
2027-Feb-23 12:21 0.132539 AU
19827526 km
16.64 km/s
2029-May-21 02:06 0.439382 AU
65730620 km
21.25 km/s
2031-Aug-18 23:07 0.177543 AU
26560048 km
15.30 km/s
2033-Sep-22 05:05 0.487024 AU
72857792 km
34.87 km/s
2046-Feb-11 10:52 0.106867 AU
15987007 km
23.01 km/s
2048-Apr-28 01:32 0.415549 AU
62165222 km
19.73 km/s
2050-Jul-13 14:34 0.352218 AU
52691015 km
15.39 km/s
2052-Sep-11 12:32 0.268060 AU
40101256 km
28.08 km/s
2065-Jan-30 05:51 0.346797 AU
51880136 km
30.74 km/s
2067-Mar-24 22:29 0.313357 AU
46877504 km
14.19 km/s
2069-Jun-11 13:42 0.427440 AU
63944134 km
20.19 km/s
2071-Aug-31 04:18 0.054774 AU
8194022 km
20.74 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
21.1

Orbit Quality

RMS
0.4339
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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