SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 GC1

2022 GC1

2022 GC1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.17 AU it takes 1.27 yr to circle the Sun.

Apollo Observations: 122
Orbital Period · P
1.27 yr
v(q)
42.1 km/s
v(Q)
18 km/s
Diameter · ≈
0.1 km
TJ
5.29
Eccentricity · e
0.4009

Orbit and dynamics

The path is an ellipse reaching 0.701 AU from the Sun at perihelion and 1.639 AU at aphelion, a radial span of 0.938 AU.

Applying Kepler's third law to a = 1.17 AU gives an orbital period of 1.27 yr, or about 462 days.

The high eccentricity (0.401) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 13.33° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 42.1 km/s at perihelion and falls to 18 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 = 22.78 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 122 observations and has a weighted RMS residual of 0.4602 arcseconds.

Condition code U = 5 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
1.17 AU
Eccentricity
0.4009
Perihelion
0.701 AU
Aphelion
1.639053 AU
Inclination
13.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
48.57°

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-Mar-27 15:02 0.414780 AU
62050145 km
9.36 km/s
2027-Jun-28 05:26 0.355724 AU
53215533 km
11.84 km/s
2032-Aug-28 13:47 0.309841 AU
46351535 km
11.69 km/s
2036-Mar-27 04:29 0.428508 AU
64103874 km
26.70 km/s
2037-Oct-23 00:12 0.046650 AU
6978793 km
14.69 km/s
2041-Apr-12 19:31 0.049593 AU
7419020 km
15.80 km/s
2042-Nov-11 09:25 0.377099 AU
56413190 km
25.49 km/s
2046-Apr-13 08:55 0.298401 AU
44640094 km
8.37 km/s
2046-Jun-01 17:51 0.294264 AU
44021328 km
9.55 km/s
2051-Aug-08 05:12 0.349151 AU
52232229 km
12.75 km/s
2051-Nov-20 09:58 0.468006 AU
70012674 km
8.99 km/s
2056-Oct-13 14:31 0.095001 AU
14211955 km
11.51 km/s
2060-Apr-06 15:45 0.168726 AU
25241048 km
19.74 km/s
2061-Nov-04 12:14 0.222350 AU
33263118 km
21.28 km/s
2065-Apr-21 14:17 0.129314 AU
19345057 km
10.24 km/s
2070-Mar-18 00:28 0.460034 AU
68820149 km
10.07 km/s
2070-Jul-14 06:56 0.367765 AU
55016812 km
12.70 km/s
2075-Sep-16 08:12 0.242965 AU
36347031 km
10.58 km/s
2079-Mar-31 15:16 0.334590 AU
50053992 km
24.37 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
22.78

Orbit Quality

RMS
0.46023
Condition
5
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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