SpaceAtlas Space Object Data
NASA JPL SBDB · 2003 YH111

2003 YH111

2003 YH111 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.417 AU it takes 1.69 yr to circle the Sun.

Apollo Observations: 116
Orbital Period · P
1.69 yr
v(q)
42.5 km/s
v(Q)
14.7 km/s
Diameter · ≈
0.04 km
TJ
4.58
Eccentricity · e
0.4859

Orbit and dynamics

The path is an ellipse reaching 0.729 AU from the Sun at perihelion and 2.106 AU at aphelion, a radial span of 1.377 AU.

Applying Kepler's third law to a = 1.417 AU gives an orbital period of 1.69 yr, or about 616 days.

The high eccentricity (0.486) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.37° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.5 km/s at perihelion and falls to 14.7 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 = 24.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 116 observations and has a weighted RMS residual of 0.3406 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
1.417 AU
Eccentricity
0.4859
Perihelion
0.729 AU
Aphelion
2.10552 AU
Inclination
4.37°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
75.26°

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
2031-Jan-05 00:08 0.033493 AU
5010555 km
11.57 km/s
2035-Dec-11 04:30 0.477513 AU
71434982 km
7.47 km/s
2036-Mar-17 19:34 0.273063 AU
40849588 km
12.61 km/s
2041-May-31 07:47 0.101864 AU
15238656 km
10.81 km/s
2046-Jun-25 07:46 0.248808 AU
37221203 km
21.83 km/s
2052-Dec-13 07:06 0.249962 AU
37393796 km
22.96 km/s
2058-Jan-07 18:35 0.036125 AU
5404294 km
10.84 km/s
2068-Jun-08 18:06 0.017269 AU
2583367 km
13.57 km/s
2073-Jul-03 05:36 0.358781 AU
53672821 km
26.65 km/s
2079-Dec-31 12:38 0.009545 AU
1427914 km
13.47 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
24.5

Orbit Quality

RMS
0.34064
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.

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