SpaceAtlas Space Object Data
NASA JPL SBDB · 2023 GE2

2023 GE2

2023 GE2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.165 AU it takes 1.26 yr to circle the Sun.

Apollo Observations: 23
Orbital Period · P
1.26 yr
v(q)
33.2 km/s
v(Q)
23 km/s
Diameter · ≈
0.01 km
TJ
5.39
Eccentricity · e
0.1821

Orbit and dynamics

The path is an ellipse reaching 0.953 AU from the Sun at perihelion and 1.377 AU at aphelion, a radial span of 0.424 AU.

Applying Kepler's third law to a = 1.165 AU gives an orbital period of 1.26 yr, or about 459 days.

An eccentricity of 0.182 makes the orbit moderately elongated.

The orbital plane is tilted 7.17° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.2 km/s at perihelion and falls to 23 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 = 27.98 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 23 observations and has a weighted RMS residual of 0.4919 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
1.165 AU
Eccentricity
0.1821
Perihelion
0.953 AU
Aphelion
1.377147 AU
Inclination
7.17°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
143.02°

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-Aug-17 21:26 0.114155 AU
17077311 km
4.33 km/s
2033-Feb-02 17:57 0.312270 AU
46714987 km
5.65 km/s
2033-Aug-24 06:39 0.146962 AU
21985246 km
10.03 km/s
2038-Sep-02 20:02 0.309462 AU
46294814 km
16.47 km/s
2052-Mar-30 01:20 0.110563 AU
16539980 km
13.92 km/s
2067-Feb-25 12:57 0.263250 AU
39381630 km
4.48 km/s
2067-Aug-20 08:53 0.111739 AU
16715891 km
6.48 km/s
2072-Aug-27 22:48 0.141457 AU
21161607 km
12.44 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
27.98

Orbit Quality

RMS
0.49185
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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