SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 FF10

2010 FF10

2010 FF10 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.38 AU it takes 3.67 yr to circle the Sun.

Apollo Observations: 196
Orbital Period · P
3.67 yr
v(q)
40.6 km/s
v(Q)
9.2 km/s
Diameter · ≈
0.16 km
TJ
3.23
Eccentricity · e
0.6314

Orbit and dynamics

Between its closest point (0.877 AU) and its farthest (3.883 AU), the heliocentric distance changes by 3.006 AU over every revolution.

One full revolution takes 3.67 yr (1,341 days), computed from the semi-major axis of 2.38 AU.

The high eccentricity (0.631) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.08° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.6 km/s at perihelion and falls to 9.2 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

The measured diameter is 0.1 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.407 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 196 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5654 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
2.38 AU
Eccentricity
0.6314
Perihelion
0.877 AU
Aphelion
3.882732 AU
Inclination
5.08°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
130.06°

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
2032-May-31 06:59 0.143104 AU
21408104 km
11.11 km/s
2043-Aug-14 14:02 0.042612 AU
6374652 km
13.79 km/s
2069-Apr-04 01:29 0.449597 AU
67258819 km
26.85 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.095 km
Albedo
0.407
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
21.8

Orbit Quality

RMS
0.56539
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.

Keep exploring

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