SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 XS2

2017 XS2

2017 XS2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.942 AU and a period of 0.91 yr.

Aten Observations: 35
Orbital Period · P
0.91 yr
v(q)
36 km/s
v(Q)
26.1 km/s
Diameter · ≈
0.02 km
TJ
6.36
Eccentricity · e
0.1591

Orbit and dynamics

The path is an ellipse reaching 0.792 AU from the Sun at perihelion and 1.092 AU at aphelion, a radial span of 0.3 AU.

Applying Kepler's third law to a = 0.942 AU gives an orbital period of 0.91 yr, or about 334 days.

An eccentricity of 0.159 makes the orbit moderately elongated.

Its inclination of 2.33° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36 km/s at perihelion and falls to 26.1 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 = 25.98 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 35 observations and has a weighted RMS residual of 0.4854 arcseconds.

Condition code U = 4 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
0.942 AU
Eccentricity
0.1591
Perihelion
0.792 AU
Aphelion
1.091872 AU
Inclination
2.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
239.91°

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
2028-Sep-05 10:59 0.182102 AU
27242054 km
4.79 km/s
2029-Jan-10 08:01 0.113931 AU
17043834 km
4.20 km/s
2029-May-13 18:59 0.174911 AU
26166304 km
4.77 km/s
2038-Nov-12 23:02 0.168870 AU
25262654 km
10.27 km/s
2040-Mar-06 01:47 0.066659 AU
9972077 km
3.53 km/s
2049-Nov-09 22:11 0.073959 AU
11064111 km
7.35 km/s
2051-Mar-14 20:53 0.045285 AU
6774508 km
5.94 km/s
2060-Nov-19 09:33 0.057044 AU
8533597 km
3.73 km/s
2062-Mar-09 09:58 0.190369 AU
28478732 km
10.79 km/s
2072-Feb-05 05:44 0.103698 AU
15512962 km
3.88 km/s
2072-Apr-16 01:30 0.133881 AU
20028244 km
2.98 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
25.98

Orbit Quality

RMS
0.48535
Condition
4
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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