SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 XH2

2022 XH2

2022 XH2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.466 AU it takes 1.78 yr to circle the Sun.

Apollo Observations: 36
Orbital Period · P
1.78 yr
v(q)
37.7 km/s
v(Q)
16.1 km/s
Diameter · ≈
0.11 km
TJ
4.51
Eccentricity · e
0.4022

Orbit and dynamics

The path is an ellipse reaching 0.876 AU from the Sun at perihelion and 2.056 AU at aphelion, a radial span of 1.18 AU.

Applying Kepler's third law to a = 1.466 AU gives an orbital period of 1.78 yr, or about 648 days.

The high eccentricity (0.402) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.25° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37.7 km/s at perihelion and falls to 16.1 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 = 22.59 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.11 km.

Observation record and orbit quality

The current orbit solution is based on 36 observations and has a weighted RMS residual of 0.4242 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
1.466 AU
Eccentricity
0.4022
Perihelion
0.876 AU
Aphelion
2.055625 AU
Inclination
9.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
305.37°

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
2030-May-22 11:01 0.297774 AU
44546396 km
18.75 km/s
2039-Jan-03 23:35 0.136344 AU
20396833 km
10.25 km/s
2039-May-30 13:50 0.483062 AU
72265064 km
5.82 km/s
2046-May-15 02:55 0.157230 AU
23521280 km
15.03 km/s
2054-Dec-26 23:41 0.190472 AU
28494232 km
14.25 km/s
2061-Nov-30 04:06 0.489734 AU
73263162 km
7.85 km/s
2062-May-06 21:52 0.037469 AU
5605337 km
11.67 km/s
2070-Dec-24 16:45 0.237704 AU
35560010 km
15.76 km/s
2078-May-07 12:03 0.040453 AU
6051623 km
11.82 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
22.59

Orbit Quality

RMS
0.42421
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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