SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 CT4

2022 CT4

2022 CT4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.286 AU it takes 1.46 yr to circle the Sun.

Apollo Observations: 54
Orbital Period · P
1.46 yr
v(q)
34 km/s
v(Q)
20.3 km/s
Diameter · ≈
0.06 km
TJ
4.99
Eccentricity · e
0.2531

Orbit and dynamics

Between its closest point (0.96 AU) and its farthest (1.611 AU), the heliocentric distance changes by 0.651 AU over every revolution.

One full revolution takes 1.46 yr (533 days), computed from the semi-major axis of 1.286 AU.

An eccentricity of 0.253 makes the orbit moderately elongated.

The orbital plane is tilted 11.41° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34 km/s at perihelion and falls to 20.3 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 = 23.79 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

Astrometry from 54 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5389 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
1.286 AU
Eccentricity
0.2531
Perihelion
0.96 AU
Aphelion
1.611487 AU
Inclination
11.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
302.07°

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
2038-Jan-24 13:46 0.362405 AU
54214964 km
5.79 km/s
2038-Jun-28 02:29 0.231648 AU
34654035 km
10.71 km/s
2041-Feb-23 19:34 0.102427 AU
15322920 km
11.44 km/s
2041-Aug-03 19:07 0.330914 AU
49504022 km
7.19 km/s
2054-Jul-09 22:30 0.421102 AU
62995970 km
18.01 km/s
2057-Mar-15 20:19 0.084024 AU
12569806 km
6.63 km/s
2057-Jul-01 03:32 0.211219 AU
31597932 km
5.18 km/s
2060-Feb-12 03:17 0.364212 AU
54485412 km
18.52 km/s
2060-Aug-25 07:42 0.446163 AU
66745021 km
8.66 km/s
2073-Jan-17 14:55 0.390425 AU
58406729 km
5.99 km/s
2073-Jun-29 18:37 0.255316 AU
38194738 km
11.69 km/s
2076-Feb-26 16:26 0.082174 AU
12293090 km
10.53 km/s
2076-Jul-31 05:03 0.319109 AU
47738022 km
6.94 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
23.79

Orbit Quality

RMS
0.53885
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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