SpaceAtlas Space Object Data
NASA JPL SBDB · 2024 GE2

2024 GE2

2024 GE2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.972 AU and a period of 0.96 yr.

Aten Observations: 35
Orbital Period · P
0.96 yr
v(q)
35.3 km/s
v(Q)
25.9 km/s
Diameter · ≈
0.01 km
TJ
6.2
Eccentricity · e
0.1537

Orbit and dynamics

The path is an ellipse reaching 0.823 AU from the Sun at perihelion and 1.122 AU at aphelion, a radial span of 0.299 AU.

Applying Kepler's third law to a = 0.972 AU gives an orbital period of 0.96 yr, or about 350 days.

An eccentricity of 0.154 makes the orbit moderately elongated.

Its inclination of 4.53° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.3 km/s at perihelion and falls to 25.9 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 = 27.97 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 35 observations and has a weighted RMS residual of 0.465 arcseconds.

Condition code U = 4 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
0.9722 AU
Eccentricity
0.1537
Perihelion
0.823 AU
Aphelion
1.121627 AU
Inclination
4.53°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
190.04°

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-Aug-13 23:43 0.368149 AU
55074351 km
14.94 km/s
2045-Apr-22 15:51 0.425946 AU
63720636 km
17.08 km/s
2046-Apr-11 12:56 0.165639 AU
24779296 km
9.38 km/s
2047-Apr-27 22:48 0.077660 AU
11617815 km
3.42 km/s
2047-Dec-08 00:24 0.170766 AU
25546279 km
5.23 km/s
2048-Sep-13 07:59 0.071247 AU
10658463 km
3.59 km/s
2049-Aug-20 16:05 0.219272 AU
32802640 km
10.56 km/s
2050-Aug-07 21:13 0.473236 AU
70795074 km
18.18 km/s
2068-Apr-14 21:11 0.263377 AU
39400668 km
12.24 km/s
2069-Apr-07 09:12 0.010434 AU
1560908 km
4.74 km/s
2070-Jan-09 08:36 0.162178 AU
24261513 km
4.58 km/s
2070-Jun-20 13:02 0.132371 AU
19802426 km
3.55 km/s
2071-Sep-02 16:37 0.055669 AU
8328025 km
5.91 km/s
2072-Aug-19 02:13 0.241611 AU
36144465 km
12.70 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
27.97

Orbit Quality

RMS
0.46496
Condition
4
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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