SpaceAtlas Space Object Data
NASA JPL SBDB · 2009 FO32

2009 FO32

2009 FO32 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.348 AU it takes 1.57 yr to circle the Sun.

Apollo Observations: 34
Orbital Period · P
1.57 yr
v(q)
44.9 km/s
v(Q)
14.7 km/s
Diameter · ≈
0.03 km
TJ
4.74
Eccentricity · e
0.508

Orbit and dynamics

The path is an ellipse reaching 0.663 AU from the Sun at perihelion and 2.033 AU at aphelion, a radial span of 1.37 AU.

Applying Kepler's third law to a = 1.348 AU gives an orbital period of 1.57 yr, or about 572 days.

The high eccentricity (0.508) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.33° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.9 km/s at perihelion and falls to 14.7 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 = 25.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 34 observations and has a weighted RMS residual of 0.44 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
1.348 AU
Eccentricity
0.508
Perihelion
0.663 AU
Aphelion
2.032784 AU
Inclination
4.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
316.71°

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-Mar-10 13:16 0.242626 AU
36296298 km
29.49 km/s
2048-Aug-14 06:44 0.279460 AU
41806648 km
12.68 km/s
2051-Oct-27 09:01 0.455837 AU
68192175 km
29.74 km/s
2056-Mar-26 18:53 0.012943 AU
1936216 km
18.65 km/s
2062-Oct-15 06:01 0.033249 AU
4973986 km
21.94 km/s
2067-Mar-14 13:59 0.174277 AU
26071512 km
26.98 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
25.7

Orbit Quality

RMS
0.43996
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.

Keep exploring

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