SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 XQ60

2017 XQ60

2017 XQ60 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.997 AU and a period of 1.00 yr.

Aten Observations: 103
Orbital Period · P
1.00 yr
v(q)
37.1 km/s
v(Q)
24 km/s
Diameter · ≈
0.04 km
TJ
5.98
Eccentricity · e
0.215

Orbit and dynamics

Between its closest point (0.783 AU) and its farthest (1.211 AU), the heliocentric distance changes by 0.428 AU over every revolution.

One full revolution takes 1.00 yr (364 days), computed from the semi-major axis of 0.997 AU.

An eccentricity of 0.215 makes the orbit moderately elongated.

A steep inclination of 27.2° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 37.1 km/s at perihelion and falls to 24 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

Astrometry from 103 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5125 arcseconds.

Condition code U = 0 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
0.9971 AU
Eccentricity
0.215
Perihelion
0.783 AU
Aphelion
1.211477 AU
Inclination
27.2°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
95.13°

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
2026-Dec-18 16:48 0.138539 AU
20725130 km
17.52 km/s
2027-Dec-18 02:08 0.166671 AU
24933587 km
18.08 km/s
2028-Dec-16 10:15 0.195914 AU
29308374 km
18.67 km/s
2029-Dec-15 16:00 0.226439 AU
33874791 km
19.31 km/s
2030-Dec-14 20:26 0.258226 AU
38629986 km
20.02 km/s
2031-Dec-14 00:24 0.290354 AU
43436341 km
20.75 km/s
2032-Dec-12 01:59 0.322940 AU
48311081 km
21.50 km/s
2033-Dec-11 02:50 0.355927 AU
53245917 km
22.31 km/s
2034-Dec-10 03:55 0.389244 AU
58230137 km
23.14 km/s
2035-Dec-09 03:31 0.422512 AU
63206970 km
23.97 km/s
2036-Dec-07 02:21 0.455832 AU
68191496 km
24.84 km/s
2037-Dec-06 01:43 0.489249 AU
73190545 km
25.72 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
0.51254
Condition
0
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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