SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 UQ

2017 UQ

2017 UQ belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.404 AU it takes 1.66 yr to circle the Sun.

Apollo Observations: 158
Orbital Period · P
1.66 yr
v(q)
33.9 km/s
v(Q)
18.7 km/s
Diameter · ≈
0.13 km
TJ
4.62
Eccentricity · e
0.2894

Orbit and dynamics

Between its closest point (0.998 AU) and its farthest (1.81 AU), the heliocentric distance changes by 0.812 AU over every revolution.

One full revolution takes 1.66 yr (608 days), computed from the semi-major axis of 1.404 AU.

An eccentricity of 0.289 makes the orbit moderately elongated.

A steep inclination of 23.81° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 33.9 km/s at perihelion and falls to 18.7 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 = 22.15 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

Astrometry from 158 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4799 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
1.404 AU
Eccentricity
0.2894
Perihelion
0.998 AU
Aphelion
1.810318 AU
Inclination
23.81°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
36.26°

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-Oct-14 23:30 0.128848 AU
19275372 km
13.92 km/s
2028-Mar-05 20:07 0.348673 AU
52160699 km
12.66 km/s
2032-Oct-13 03:31 0.150940 AU
22580314 km
14.73 km/s
2033-Mar-08 13:00 0.353541 AU
52888943 km
12.50 km/s
2037-Oct-11 21:43 0.196035 AU
29326358 km
15.82 km/s
2038-Mar-11 15:43 0.365943 AU
54744273 km
12.42 km/s
2042-Oct-10 04:12 0.258259 AU
38635041 km
17.21 km/s
2043-Mar-15 04:02 0.386272 AU
57785542 km
12.42 km/s
2047-Oct-07 23:27 0.332133 AU
49686360 km
18.86 km/s
2048-Mar-17 23:45 0.413642 AU
61880015 km
12.49 km/s
2052-Oct-04 09:53 0.413357 AU
61837375 km
20.74 km/s
2053-Mar-22 00:46 0.446597 AU
66809981 km
12.61 km/s
2057-Oct-01 12:29 0.499671 AU
74749737 km
22.83 km/s
2058-Mar-26 06:06 0.483701 AU
72360640 km
12.74 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
22.15

Orbit Quality

RMS
0.47993
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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