SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 CK8

2022 CK8

2022 CK8 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.947 AU it takes 2.72 yr to circle the Sun.

Apollo Observations: 72
Orbital Period · P
2.72 yr
v(q)
51.4 km/s
v(Q)
8.9 km/s
Diameter · ≈
0.34 km
TJ
3.53
Eccentricity · e
0.706

Orbit and dynamics

The path is an ellipse reaching 0.572 AU from the Sun at perihelion and 3.322 AU at aphelion, a radial span of 2.75 AU.

Applying Kepler's third law to a = 1.947 AU gives an orbital period of 2.72 yr, or about 992 days.

The high eccentricity (0.706) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.73° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 51.4 km/s at perihelion and falls to 8.9 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 = 20.07 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.34 km.

Observation record and orbit quality

The current orbit solution is based on 72 observations and has a weighted RMS residual of 0.601 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
1.947 AU
Eccentricity
0.706
Perihelion
0.572 AU
Aphelion
3.321582 AU
Inclination
6.73°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
161.98°

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-Oct-07 19:32 0.460083 AU
68827380 km
35.36 km/s
2033-Apr-15 06:14 0.321054 AU
48028952 km
16.14 km/s
2041-Aug-18 12:28 0.296301 AU
44325943 km
14.50 km/s
2044-Feb-18 12:52 0.417412 AU
62443959 km
34.02 km/s
2052-May-20 04:21 0.422817 AU
63252460 km
21.16 km/s
2060-Sep-10 15:45 0.127223 AU
19032336 km
19.41 km/s
2063-Feb-27 09:35 0.238621 AU
35697224 km
28.32 km/s
2071-Jun-03 07:51 0.440195 AU
65852180 km
22.19 km/s
2079-Sep-22 20:16 0.161799 AU
24204788 km
25.60 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
20.07

Orbit Quality

RMS
0.60102
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.