SpaceAtlas Space Object Data
NASA JPL SBDB · 2009 DB12

2009 DB12

2009 DB12 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.172 AU it takes 1.27 yr to circle the Sun.

Apollo Observations: 62
Orbital Period · P
1.27 yr
v(q)
52.2 km/s
v(Q)
14.5 km/s
Diameter · ≈
0.2 km
TJ
5.14
Eccentricity · e
0.5658

Orbit and dynamics

The path is an ellipse reaching 0.509 AU from the Sun at perihelion and 1.835 AU at aphelion, a radial span of 1.326 AU.

Applying Kepler's third law to a = 1.172 AU gives an orbital period of 1.27 yr, or about 463 days.

The high eccentricity (0.566) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 26.88° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 52.2 km/s at perihelion and falls to 14.5 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 = 21.27 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

The current orbit solution is based on 62 observations and has a weighted RMS residual of 0.6606 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
1.172 AU
Eccentricity
0.5658
Perihelion
0.509 AU
Aphelion
1.835118 AU
Inclination
26.88°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
287.5°

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-Feb-12 05:05 0.175434 AU
26244538 km
25.02 km/s
2040-Jul-18 21:24 0.330423 AU
49430623 km
22.64 km/s
2042-Feb-05 03:53 0.174411 AU
26091459 km
18.66 km/s
2045-Sep-01 14:13 0.440889 AU
65956042 km
23.94 km/s
2047-Feb-18 13:39 0.327297 AU
48962943 km
29.91 km/s
2054-Jun-27 23:07 0.399909 AU
59825516 km
27.06 km/s
2056-Feb-09 21:43 0.402129 AU
60157673 km
15.86 km/s
2059-Aug-05 09:28 0.355687 AU
53210045 km
22.08 km/s
2061-Feb-08 12:55 0.117549 AU
17585058 km
22.50 km/s
2064-Sep-18 20:49 0.495121 AU
74069087 km
25.25 km/s
2066-Feb-25 12:52 0.488790 AU
73121949 km
34.97 km/s
2073-Jul-11 03:45 0.337082 AU
50426799 km
23.73 km/s
2075-Feb-05 08:40 0.250712 AU
37505972 km
17.14 km/s
2078-Aug-23 19:35 0.411094 AU
61498790 km
23.14 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
21.27

Orbit Quality

RMS
0.66056
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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