SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 CQ2

2022 CQ2

2022 CQ2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.688 AU and a period of 0.57 yr.

Aten Observations: 47
Orbital Period · P
0.57 yr
v(q)
65.6 km/s
v(Q)
19.6 km/s
Diameter · ≈
0.04 km
TJ
8.17
Eccentricity · e
0.5399

Orbit and dynamics

Between its closest point (0.317 AU) and its farthest (1.059 AU), the heliocentric distance changes by 0.742 AU over every revolution.

One full revolution takes 0.57 yr (208 days), computed from the semi-major axis of 0.688 AU.

The high eccentricity (0.54) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 5.51° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 65.6 km/s at perihelion and falls to 19.6 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 = 24.87 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 47 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4422 arcseconds.

Condition code U = 1 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
0.688 AU
Eccentricity
0.5399
Perihelion
0.317 AU
Aphelion
1.059451 AU
Inclination
5.51°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
5.75°

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-Feb-06 08:39 0.077202 AU
11549295 km
10.89 km/s
2034-Feb-09 20:39 0.080217 AU
12000324 km
10.79 km/s
2038-Feb-13 06:39 0.080572 AU
12053462 km
10.75 km/s
2042-Feb-16 21:52 0.078442 AU
11734768 km
10.77 km/s
2046-Feb-20 05:09 0.073927 AU
11059252 km
10.79 km/s
2050-Feb-23 12:02 0.066522 AU
9951610 km
10.90 km/s
2054-Feb-26 06:51 0.057521 AU
8605065 km
11.03 km/s
2058-Feb-28 16:06 0.047171 AU
7056643 km
11.23 km/s
2062-Mar-02 06:27 0.038247 AU
5721667 km
11.42 km/s
2066-Mar-03 03:52 0.032253 AU
4825044 km
11.55 km/s
2070-Mar-03 05:29 0.031975 AU
4783339 km
11.57 km/s
2074-Mar-02 12:52 0.036635 AU
5480471 km
11.46 km/s
2078-Mar-01 01:38 0.045269 AU
6772101 km
11.25 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
24.87

Orbit Quality

RMS
0.44222
Condition
1
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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