SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 RV16

2012 RV16

2012 RV16 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.768 AU it takes 4.61 yr to circle the Sun.

Apollo Observations: 301
Orbital Period · P
4.61 yr
v(q)
40.3 km/s
v(Q)
7.9 km/s
Diameter · ≈
0.42 km
TJ
2.9
Eccentricity · e
0.671

Orbit and dynamics

Between its closest point (0.911 AU) and its farthest (4.625 AU), the heliocentric distance changes by 3.714 AU over every revolution.

One full revolution takes 4.61 yr (1,682 days), computed from the semi-major axis of 2.768 AU.

The high eccentricity (0.671) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 20.22° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 40.3 km/s at perihelion and falls to 7.9 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 = 19.63 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.42 km.

Observation record and orbit quality

Astrometry from 301 individual observations underpins this orbit; the fit leaves an RMS residual of 0.357 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
2.768 AU
Eccentricity
0.671
Perihelion
0.911 AU
Aphelion
4.625328 AU
Inclination
20.22°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
339.42°

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
2035-Oct-15 21:08 0.131596 AU
19686488 km
17.34 km/s
2058-Oct-03 20:04 0.262031 AU
39199230 km
22.57 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
19.63

Orbit Quality

RMS
0.35705
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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