SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 UY68

2012 UY68

2012 UY68 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.175 AU it takes 1.27 yr to circle the Sun.

Apollo Observations: 45
Orbital Period · P
1.27 yr
v(q)
34.7 km/s
v(Q)
21.8 km/s
Diameter · ≈
0.04 km
TJ
5.35
Eccentricity · e
0.2281

Orbit and dynamics

Between its closest point (0.907 AU) and its farthest (1.443 AU), the heliocentric distance changes by 0.536 AU over every revolution.

One full revolution takes 1.27 yr (465 days), computed from the semi-major axis of 1.175 AU.

An eccentricity of 0.228 makes the orbit moderately elongated.

Its inclination of 2.9° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.7 km/s at perihelion and falls to 21.8 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 = 25 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 45 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5477 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.175 AU
Eccentricity
0.2281
Perihelion
0.907 AU
Aphelion
1.443018 AU
Inclination
2.9°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
200.11°

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
2031-Aug-05 07:12 0.398179 AU
59566677 km
7.07 km/s
2032-Mar-30 15:13 0.372411 AU
55711837 km
17.08 km/s
2035-Oct-15 15:58 0.412696 AU
61738430 km
17.68 km/s
2036-Jun-11 10:30 0.402250 AU
60175722 km
7.19 km/s
2045-Jul-22 12:17 0.417752 AU
62494874 km
7.44 km/s
2049-Oct-21 04:42 0.273012 AU
40842018 km
14.07 km/s
2050-May-31 16:44 0.374611 AU
56040971 km
6.78 km/s
2054-Sep-15 23:49 0.280544 AU
41968727 km
4.69 km/s
2055-Mar-07 04:20 0.050572 AU
7565433 km
5.90 km/s
2059-Jul-13 02:26 0.429311 AU
64223954 km
7.60 km/s
2063-Oct-30 23:24 0.071378 AU
10678030 km
9.54 km/s
2064-May-15 06:43 0.302348 AU
45230648 km
5.96 km/s
2068-Aug-24 03:32 0.328200 AU
49098086 km
6.20 km/s
2069-Mar-20 14:19 0.112537 AU
16835279 km
11.21 km/s
2073-Jun-28 22:44 0.419050 AU
62689016 km
7.58 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
25.0

Orbit Quality

RMS
0.54772
Condition
7
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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