SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 OD22

2015 OD22

2015 OD22 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.221 AU it takes 1.35 yr to circle the Sun.

Apollo Observations: 40
Orbital Period · P
1.35 yr
v(q)
49.7 km/s
v(Q)
14.6 km/s
Diameter · ≈
0.2 km
TJ
4.97
Eccentricity · e
0.5455

Orbit and dynamics

Between its closest point (0.555 AU) and its farthest (1.887 AU), the heliocentric distance changes by 1.332 AU over every revolution.

One full revolution takes 1.35 yr (493 days), computed from the semi-major axis of 1.221 AU.

The high eccentricity (0.545) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 28.76° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 49.7 km/s at perihelion and falls to 14.6 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 = 21.21 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

Astrometry from 40 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4864 arcseconds.

Condition code U = 6 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
1.221 AU
Eccentricity
0.5455
Perihelion
0.555 AU
Aphelion
1.887056 AU
Inclination
28.76°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
297.29°

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-Jan-28 10:32 0.359453 AU
53773355 km
24.18 km/s
2032-Feb-24 00:17 0.344988 AU
51609484 km
23.80 km/s
2034-Aug-07 12:31 0.366333 AU
54802689 km
28.05 km/s
2036-Mar-18 17:53 0.414686 AU
62036101 km
26.82 km/s
2038-Aug-15 09:31 0.255436 AU
38212610 km
21.31 km/s
2042-Aug-15 23:38 0.294313 AU
44028614 km
16.99 km/s
2046-Aug-08 02:45 0.442826 AU
66245855 km
16.10 km/s
2050-Dec-15 04:01 0.469220 AU
70194330 km
25.23 km/s
2055-Jan-11 08:43 0.394418 AU
59004138 km
25.06 km/s
2065-Aug-10 20:48 0.274804 AU
41110164 km
25.35 km/s
2067-Mar-27 10:56 0.428997 AU
64176970 km
28.86 km/s
2069-Aug-16 16:32 0.256987 AU
38444641 km
19.27 km/s
2073-Aug-13 11:38 0.318527 AU
47650994 km
16.33 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
21.21

Orbit Quality

RMS
0.48645
Condition
6
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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