SpaceAtlas Space Object Data
NASA JPL SBDB · 2000 AG6

2000 AG6

2000 AG6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.017 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 74
Orbital Period · P
1.03 yr
v(q)
35.8 km/s
v(Q)
24.4 km/s
Diameter · ≈
0.03 km
TJ
5.98
Eccentricity · e
0.1891

Orbit and dynamics

The path is an ellipse reaching 0.824 AU from the Sun at perihelion and 1.209 AU at aphelion, a radial span of 0.385 AU.

Applying Kepler's third law to a = 1.017 AU gives an orbital period of 1.03 yr, or about 375 days.

An eccentricity of 0.189 makes the orbit moderately elongated.

Its inclination of 2.44° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.8 km/s at perihelion and falls to 24.4 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 = 25.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 74 observations and has a weighted RMS residual of 0.5695 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
1.017 AU
Eccentricity
0.1891
Perihelion
0.824 AU
Aphelion
1.209315 AU
Inclination
2.44°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
203.88°

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
2037-Dec-22 19:15 0.378782 AU
56665039 km
18.32 km/s
2038-Dec-29 19:08 0.223903 AU
33495464 km
13.64 km/s
2040-Jan-05 13:12 0.068376 AU
10228859 km
9.00 km/s
2041-Jan-10 11:00 0.012035 AU
1800440 km
4.53 km/s
2041-Nov-28 14:05 0.158021 AU
23639593 km
4.58 km/s
2042-Mar-10 12:07 0.151106 AU
22605193 km
5.22 km/s
2042-Oct-28 19:19 0.211034 AU
31570216 km
5.40 km/s
2043-Apr-19 07:16 0.181113 AU
27094141 km
6.04 km/s
2043-Oct-01 09:22 0.207297 AU
31011204 km
5.30 km/s
2044-May-29 14:31 0.150399 AU
22499307 km
4.84 km/s
2044-Aug-27 19:11 0.160570 AU
24020866 km
4.17 km/s
2045-Jul-20 15:18 0.023022 AU
3444008 km
5.06 km/s
2046-Jul-27 09:36 0.095663 AU
14311038 km
9.05 km/s
2047-Aug-03 02:24 0.231756 AU
34670212 km
13.25 km/s
2048-Aug-08 13:08 0.367300 AU
54947249 km
17.43 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
25.3

Orbit Quality

RMS
0.56945
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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