SpaceAtlas Space Object Data
NASA JPL SBDB · 2006 UQ17

2006 UQ17

2006 UQ17 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.624 AU it takes 2.07 yr to circle the Sun.

Apollo Observations: 650
Orbital Period · P
2.07 yr
v(q)
34.9 km/s
v(Q)
15.6 km/s
Diameter · ≈
0.15 km
TJ
4.24
Eccentricity · e
0.3809

Orbit and dynamics

Between its closest point (1.005 AU) and its farthest (2.243 AU), the heliocentric distance changes by 1.238 AU over every revolution.

One full revolution takes 2.07 yr (756 days), computed from the semi-major axis of 1.624 AU.

An eccentricity of 0.381 makes the orbit moderately elongated.

Its inclination of 1.74° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.9 km/s at perihelion and falls to 15.6 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 21.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.15 km.

Observation record and orbit quality

Astrometry from 650 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4686 arcseconds.

Condition code U = 1 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
1.624 AU
Eccentricity
0.3809
Perihelion
1.005 AU
Aphelion
2.242582 AU
Inclination
1.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
144.63°

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-Nov-18 05:49 0.157929 AU
23625855 km
9.56 km/s
2038-Feb-01 15:31 0.205269 AU
30707844 km
11.00 km/s
2064-Oct-31 06:37 0.418137 AU
62552447 km
17.55 km/s
2066-Dec-17 10:31 0.023731 AU
3550074 km
4.86 km/s
2068-Oct-14 10:06 0.458287 AU
68558708 km
3.44 km/s
2069-Feb-11 15:54 0.350770 AU
52474405 km
15.48 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
21.9

Orbit Quality

RMS
0.4686
Condition
1
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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