SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 DY32

2012 DY32

2012 DY32 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.084 AU it takes 1.13 yr to circle the Sun.

Apollo Observations: 78
Orbital Period · P
1.13 yr
v(q)
33.8 km/s
v(Q)
24.2 km/s
Diameter · ≈
0.1 km
TJ
5.69
Eccentricity · e
0.1659

Orbit and dynamics

The path is an ellipse reaching 0.904 AU from the Sun at perihelion and 1.264 AU at aphelion, a radial span of 0.36 AU.

Applying Kepler's third law to a = 1.084 AU gives an orbital period of 1.13 yr, or about 412 days.

An eccentricity of 0.166 makes the orbit moderately elongated.

The orbital plane is tilted 9.54° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.8 km/s at perihelion and falls to 24.2 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 = 22.69 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 78 observations and has a weighted RMS residual of 0.4903 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
1.084 AU
Eccentricity
0.1659
Perihelion
0.904 AU
Aphelion
1.263836 AU
Inclination
9.54°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
311.05°

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
2028-Aug-30 01:20 0.080286 AU
12010573 km
8.28 km/s
2029-Apr-13 21:33 0.278344 AU
41639628 km
5.73 km/s
2030-Feb-20 05:05 0.408443 AU
61102213 km
17.09 km/s
2037-Sep-06 09:22 0.051596 AU
7718584 km
5.71 km/s
2038-Mar-20 12:55 0.222201 AU
33240783 km
5.68 km/s
2046-Jul-26 13:44 0.241455 AU
36121116 km
4.65 km/s
2047-Feb-15 02:10 0.090547 AU
13545624 km
5.72 km/s
2054-Aug-16 14:44 0.359843 AU
53831781 km
15.67 km/s
2055-Jun-04 23:05 0.308635 AU
46171109 km
5.04 km/s
2056-Feb-11 05:05 0.144867 AU
21671850 km
9.45 km/s
2063-Aug-27 06:21 0.150653 AU
22537362 km
10.02 km/s
2064-Apr-25 09:16 0.297549 AU
44512689 km
5.65 km/s
2065-Feb-17 05:32 0.348430 AU
52124337 km
15.35 km/s
2072-Sep-05 14:48 0.043770 AU
6547938 km
5.84 km/s
2073-Mar-21 00:31 0.225696 AU
33763645 km
5.70 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
22.69

Orbit Quality

RMS
0.49027
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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