SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 GC3

2022 GC3

2022 GC3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.116 AU it takes 1.18 yr to circle the Sun.

Apollo Observations: 18
Orbital Period · P
1.18 yr
v(q)
33.6 km/s
v(Q)
23.6 km/s
Diameter · ≈
0.01 km
TJ
5.56
Eccentricity · e
0.175

Orbit and dynamics

The path is an ellipse reaching 0.921 AU from the Sun at perihelion and 1.311 AU at aphelion, a radial span of 0.39 AU.

Applying Kepler's third law to a = 1.116 AU gives an orbital period of 1.18 yr, or about 431 days.

An eccentricity of 0.175 makes the orbit moderately elongated.

The orbital plane is tilted 9.17° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.6 km/s at perihelion and falls to 23.6 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 = 28.71 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 18 observations and has a weighted RMS residual of 0.6825 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.116 AU
Eccentricity
0.175
Perihelion
0.921 AU
Aphelion
1.3113 AU
Inclination
9.17°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
245.51°

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
2027-Nov-01 17:01 0.392995 AU
58791243 km
16.95 km/s
2028-Aug-01 18:29 0.334726 AU
50074346 km
6.09 km/s
2029-Apr-27 09:39 0.425286 AU
63621885 km
18.54 km/s
2034-Oct-31 21:45 0.116703 AU
17458526 km
5.58 km/s
2042-Apr-17 17:36 0.156902 AU
23472212 km
13.28 km/s
2047-Nov-10 02:49 0.111740 AU
16716089 km
9.14 km/s
2060-Nov-05 03:55 0.279311 AU
41784372 km
13.96 km/s
2061-Jul-18 03:56 0.336307 AU
50310789 km
5.75 km/s
2073-Oct-29 00:47 0.434595 AU
65014444 km
19.10 km/s
2074-Aug-13 00:14 0.322689 AU
48273616 km
6.27 km/s
2075-Apr-23 19:15 0.325739 AU
48729897 km
16.28 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
28.71

Orbit Quality

RMS
0.68251
Condition
7
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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