SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 XC

2018 XC

2018 XC is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.79 AU and a period of 0.70 yr.

Aten Observations: 48
Orbital Period · P
0.70 yr
v(q)
51.4 km/s
v(Q)
21.8 km/s
Diameter · ≈
0.03 km
TJ
7.25
Eccentricity · e
0.4035

Orbit and dynamics

The path is an ellipse reaching 0.471 AU from the Sun at perihelion and 1.109 AU at aphelion, a radial span of 0.638 AU.

Applying Kepler's third law to a = 0.79 AU gives an orbital period of 0.70 yr, or about 257 days.

The high eccentricity (0.404) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 21.33° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 51.4 km/s at perihelion and falls to 21.8 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 = 25.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 48 observations and has a weighted RMS residual of 0.3934 arcseconds.

Condition code U = 6 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
0.7901 AU
Eccentricity
0.4035
Perihelion
0.471 AU
Aphelion
1.108905 AU
Inclination
21.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
9.67°

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-Dec-28 08:36 0.262285 AU
39237262 km
12.38 km/s
2032-Dec-03 21:37 0.213830 AU
31988445 km
20.49 km/s
2036-Jan-26 06:55 0.480402 AU
71867056 km
22.39 km/s
2037-Dec-14 02:16 0.181396 AU
27136437 km
12.26 km/s
2038-Apr-05 03:00 0.422667 AU
63230149 km
14.50 km/s
2039-Dec-08 20:16 0.327936 AU
49058463 km
24.35 km/s
2043-Jan-29 01:37 0.394761 AU
59055385 km
18.17 km/s
2044-Dec-04 07:23 0.077709 AU
11625117 km
12.69 km/s
2045-Apr-21 00:30 0.447069 AU
66880559 km
17.82 km/s
2046-Dec-13 03:02 0.437464 AU
65443674 km
28.15 km/s
2050-Jan-26 23:40 0.341919 AU
51150401 km
14.52 km/s
2051-Dec-01 10:16 0.012720 AU
1902830 km
14.28 km/s
2052-May-03 05:17 0.469679 AU
70262961 km
20.17 km/s
2058-Dec-01 04:03 0.022163 AU
3315594 km
16.09 km/s
2065-Dec-02 14:48 0.044638 AU
6677757 km
18.68 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
25.7

Orbit Quality

RMS
0.39341
Condition
6
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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