SpaceAtlas Space Object Data
NASA JPL SBDB · 2005 YO3

2005 YO3

2005 YO3 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.759 AU and a period of 0.66 yr.

Aten Observations: 21
Orbital Period · P
0.66 yr
v(q)
50.6 km/s
v(Q)
23.1 km/s
Diameter · ≈
0.03 km
TJ
7.54
Eccentricity · e
0.3733

Orbit and dynamics

Between its closest point (0.476 AU) and its farthest (1.043 AU), the heliocentric distance changes by 0.567 AU over every revolution.

One full revolution takes 0.66 yr (242 days), computed from the semi-major axis of 0.759 AU.

An eccentricity of 0.373 makes the orbit moderately elongated.

The orbital plane is tilted 12.8° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 50.6 km/s at perihelion and falls to 23.1 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 = 25.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 21 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5684 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
0.7595 AU
Eccentricity
0.3733
Perihelion
0.476 AU
Aphelion
1.043021 AU
Inclination
12.8°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
98.35°

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
2040-Dec-29 13:48 0.233506 AU
34932015 km
25.27 km/s
2042-Dec-27 01:55 0.141244 AU
21129730 km
22.54 km/s
2044-Dec-23 19:17 0.054977 AU
8224378 km
19.86 km/s
2046-Dec-21 23:38 0.031105 AU
4653196 km
17.23 km/s
2048-Dec-19 22:00 0.028554 AU
4271689 km
14.76 km/s
2050-Dec-20 02:17 0.023340 AU
3491542 km
12.54 km/s
2059-Jan-12 12:36 0.083583 AU
12503826 km
9.20 km/s
2061-Jan-22 18:23 0.128668 AU
19248531 km
9.56 km/s
2063-Feb-01 01:03 0.146232 AU
21875942 km
10.63 km/s
2065-Feb-04 19:06 0.160889 AU
24068712 km
12.57 km/s
2067-Feb-06 00:15 0.170599 AU
25521195 km
15.00 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
25.1

Orbit Quality

RMS
0.56839
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.