SpaceAtlas Space Object Data
NASA JPL SBDB · 2011 CC22

2011 CC22

2011 CC22 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.123 AU it takes 1.19 yr to circle the Sun.

Apollo Observations: 62
Orbital Period · P
1.19 yr
v(q)
31.6 km/s
v(Q)
25 km/s
Diameter · ≈
0.2 km
TJ
5.39
Eccentricity · e
0.1152

Orbit and dynamics

The path is an ellipse reaching 0.993 AU from the Sun at perihelion and 1.252 AU at aphelion, a radial span of 0.259 AU.

Applying Kepler's third law to a = 1.123 AU gives an orbital period of 1.19 yr, or about 435 days.

An eccentricity of 0.115 makes the orbit moderately elongated.

A steep inclination of 34.83° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 31.6 km/s at perihelion and falls to 25 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 = 21.22 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 0.7366 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
1.123 AU
Eccentricity
0.1152
Perihelion
0.993 AU
Aphelion
1.25237 AU
Inclination
34.83°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
163.55°

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
2030-Jan-29 16:16 0.272695 AU
40794611 km
17.28 km/s
2036-Feb-06 04:41 0.312040 AU
46680583 km
17.69 km/s
2036-Aug-12 12:29 0.221585 AU
33148649 km
19.68 km/s
2042-Feb-12 12:51 0.477022 AU
71361418 km
19.29 km/s
2042-Jul-29 19:25 0.096499 AU
14436099 km
18.44 km/s
2048-Jul-14 09:41 0.419390 AU
62739894 km
21.59 km/s
2049-Jan-25 06:46 0.328645 AU
49164570 km
17.51 km/s
2055-Feb-02 06:36 0.267374 AU
39998617 km
17.33 km/s
2055-Aug-20 22:20 0.391357 AU
58546164 km
21.99 km/s
2061-Feb-08 20:19 0.384017 AU
57448149 km
18.32 km/s
2061-Aug-05 22:04 0.069615 AU
10414257 km
18.53 km/s
2067-Jul-23 06:34 0.244864 AU
36631131 km
19.39 km/s
2068-Jan-21 13:17 0.416151 AU
62255292 km
18.02 km/s
2074-Jan-28 19:46 0.281997 AU
42186135 km
17.31 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
21.22

Orbit Quality

RMS
0.73662
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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