SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 QQ50

2012 QQ50

2012 QQ50 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.717 AU it takes 2.25 yr to circle the Sun.

Apollo Observations: 169
Orbital Period · P
2.25 yr
v(q)
39.6 km/s
v(Q)
13 km/s
Diameter · ≈
0.39 km
TJ
4.01
Eccentricity · e
0.5046

Orbit and dynamics

Between its closest point (0.85 AU) and its farthest (2.583 AU), the heliocentric distance changes by 1.733 AU over every revolution.

One full revolution takes 2.25 yr (822 days), computed from the semi-major axis of 1.717 AU.

The high eccentricity (0.505) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.42° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 39.6 km/s at perihelion and falls to 13 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 = 19.82 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.39 km.

Observation record and orbit quality

Astrometry from 169 individual observations underpins this orbit; the fit leaves an RMS residual of 0.415 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
1.717 AU
Eccentricity
0.5046
Perihelion
0.85 AU
Aphelion
2.583398 AU
Inclination
9.42°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
354.87°

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-Dec-21 09:06 0.148188 AU
22168535 km
10.76 km/s
2039-Dec-22 00:07 0.147302 AU
22036047 km
10.72 km/s
2048-Dec-20 18:09 0.147739 AU
22101509 km
10.76 km/s
2057-Dec-19 21:21 0.146627 AU
21935131 km
10.74 km/s
2066-Dec-19 17:40 0.147479 AU
22062495 km
10.77 km/s
2075-Dec-22 06:08 0.147762 AU
22104845 km
10.73 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
19.82

Orbit Quality

RMS
0.41497
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.

Keep exploring

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