SpaceAtlas Space Object Data
NASA JPL SBDB · 2000 AE205

2000 AE205

2000 AE205 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: 84
Orbital Period · P
1.26 yr
v(q)
31.7 km/s
v(Q)
24 km/s
Diameter · ≈
0.08 km
TJ
5.4
Eccentricity · e
0.1376

Orbit and dynamics

The path is an ellipse reaching 1.004 AU from the Sun at perihelion and 1.325 AU at aphelion, a radial span of 0.321 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 0.138 makes the orbit moderately elongated.

Its inclination of 4.46° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 31.7 km/s at perihelion and falls to 24 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.32 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.08 km.

Observation record and orbit quality

The current orbit solution is based on 84 observations and has a weighted RMS residual of 0.4905 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
0.1376
Perihelion
1.004 AU
Aphelion
1.325304 AU
Inclination
4.46°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
45.52°

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
2029-May-04 13:29 0.314010 AU
46975252 km
5.51 km/s
2033-Sep-24 23:48 0.496215 AU
74232710 km
16.24 km/s
2034-Apr-13 07:34 0.295027 AU
44135351 km
4.98 km/s
2038-Oct-06 00:33 0.335501 AU
50190248 km
11.36 km/s
2039-Mar-19 11:59 0.255737 AU
38257673 km
3.99 km/s
2043-Oct-20 19:47 0.185903 AU
27810656 km
6.64 km/s
2044-Feb-11 10:13 0.188502 AU
28199443 km
2.41 km/s
2048-Nov-28 19:48 0.068052 AU
10180450 km
2.85 km/s
2053-Dec-10 07:10 0.033410 AU
4998012 km
2.80 km/s
2058-Dec-03 13:21 0.058039 AU
8682454 km
2.76 km/s
2063-Oct-26 02:24 0.172961 AU
25874559 km
6.10 km/s
2064-Feb-08 20:04 0.177892 AU
26612196 km
2.23 km/s
2068-Oct-08 16:25 0.319229 AU
47755962 km
10.78 km/s
2069-Mar-19 17:10 0.244437 AU
36567318 km
3.82 km/s
2073-Sep-27 20:28 0.477376 AU
71414362 km
15.60 km/s
2074-Apr-15 04:58 0.281697 AU
42141222 km
4.80 km/s
2079-May-07 17:13 0.298419 AU
44642859 km
5.34 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
23.32

Orbit Quality

RMS
0.49052
Condition
1
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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