SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 GE

2022 GE

2022 GE belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.225 AU it takes 1.36 yr to circle the Sun.

Apollo Observations: 37
Orbital Period · P
1.36 yr
v(q)
42.2 km/s
v(Q)
17.2 km/s
Diameter · ≈
0.01 km
TJ
5.13
Eccentricity · e
0.4213

Orbit and dynamics

Between its closest point (0.709 AU) and its farthest (1.741 AU), the heliocentric distance changes by 1.032 AU over every revolution.

One full revolution takes 1.36 yr (495 days), computed from the semi-major axis of 1.225 AU.

The high eccentricity (0.421) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.38° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.2 km/s at perihelion and falls to 17.2 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 = 27.15 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 37 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5161 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
1.225 AU
Eccentricity
0.4213
Perihelion
0.709 AU
Aphelion
1.741093 AU
Inclination
4.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
78.09°

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
2028-Sep-13 04:40 0.277984 AU
41585883 km
22.71 km/s
2032-Oct-05 13:54 0.003970 AU
593856 km
10.48 km/s
2037-May-01 19:43 0.414913 AU
62070173 km
8.81 km/s
2045-Apr-11 11:07 0.236231 AU
35339628 km
21.01 km/s
2047-Sep-07 20:12 0.442470 AU
66192538 km
26.46 km/s
2051-Sep-26 07:45 0.104247 AU
15595077 km
15.36 km/s
2055-Nov-14 18:29 0.208043 AU
31122755 km
9.28 km/s
2060-Apr-21 05:42 0.351658 AU
52607233 km
7.65 km/s
2064-Mar-21 09:16 0.004394 AU
657371 km
9.77 km/s
2068-Apr-08 12:03 0.123410 AU
18461804 km
19.14 km/s
2074-Sep-16 17:25 0.201335 AU
30119304 km
20.89 km/s
2078-Oct-02 18:21 0.002823 AU
422288 km
11.87 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
27.15

Orbit Quality

RMS
0.5161
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.

Keep exploring

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