SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 AF40

2010 AF40

2010 AF40 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.238 AU it takes 1.38 yr to circle the Sun.

Apollo Observations: 73
Orbital Period · P
1.38 yr
v(q)
44.3 km/s
v(Q)
16.2 km/s
Diameter · ≈
0.04 km
TJ
5.07
Eccentricity · e
0.4644

Orbit and dynamics

Between its closest point (0.663 AU) and its farthest (1.813 AU), the heliocentric distance changes by 1.15 AU over every revolution.

One full revolution takes 1.38 yr (503 days), computed from the semi-major axis of 1.238 AU.

The high eccentricity (0.464) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.3° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.3 km/s at perihelion and falls to 16.2 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 = 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 73 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4445 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.238 AU
Eccentricity
0.4644
Perihelion
0.663 AU
Aphelion
1.812927 AU
Inclination
4.3°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
277.95°

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-Mar-08 19:03 0.274904 AU
41125003 km
11.18 km/s
2036-Jul-19 03:13 0.146912 AU
21977685 km
9.88 km/s
2039-Jan-02 17:11 0.386701 AU
57849717 km
26.48 km/s
2043-Jan-03 13:30 0.413701 AU
61888729 km
8.52 km/s
2043-Mar-28 12:34 0.316870 AU
47403142 km
13.31 km/s
2047-Jul-29 03:41 0.016598 AU
2483004 km
13.26 km/s
2050-Jan-08 04:28 0.271643 AU
40637286 km
22.59 km/s
2054-Apr-15 09:28 0.340897 AU
50997435 km
14.50 km/s
2058-Aug-04 17:35 0.012518 AU
1872730 km
16.90 km/s
2061-Jan-14 01:22 0.039005 AU
5835074 km
18.67 km/s
2069-Aug-10 20:49 0.077595 AU
11608107 km
20.70 km/s
2072-Jan-21 14:50 0.002771 AU
414512 km
14.56 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
0.44453
Condition
5
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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