SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 XC352

2015 XC352

2015 XC352 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.015 AU it takes 1.02 yr to circle the Sun.

Apollo Observations: 87
Orbital Period · P
1.02 yr
v(q)
34.2 km/s
v(Q)
25.5 km/s
Diameter · ≈
0.02 km
TJ
6
Eccentricity · e
0.1455

Orbit and dynamics

Between its closest point (0.867 AU) and its farthest (1.163 AU), the heliocentric distance changes by 0.296 AU over every revolution.

One full revolution takes 1.02 yr (373 days), computed from the semi-major axis of 1.015 AU.

An eccentricity of 0.145 makes the orbit moderately elongated.

Its inclination of 4.48° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.2 km/s at perihelion and falls to 25.5 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 = 25.82 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 87 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4318 arcseconds.

Condition code U = 1 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
1.015 AU
Eccentricity
0.1455
Perihelion
0.867 AU
Aphelion
1.162682 AU
Inclination
4.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
5.35°

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
2057-Dec-07 15:34 0.453764 AU
67882114 km
18.22 km/s
2058-Dec-14 06:51 0.314941 AU
47114463 km
14.05 km/s
2059-Dec-20 16:37 0.175123 AU
26197957 km
9.87 km/s
2060-Dec-26 05:01 0.037116 AU
5552488 km
5.89 km/s
2062-Jan-04 08:40 0.080586 AU
12055471 km
3.02 km/s
2062-Nov-01 17:18 0.160100 AU
23950623 km
3.87 km/s
2063-Mar-11 23:58 0.144966 AU
21686581 km
4.28 km/s
2063-Sep-29 02:36 0.178820 AU
26751025 km
4.15 km/s
2064-Apr-23 01:28 0.142794 AU
21361621 km
4.14 km/s
2064-Aug-24 13:27 0.156566 AU
23421932 km
3.70 km/s
2065-Jun-27 13:49 0.070633 AU
10566493 km
3.18 km/s
2066-Jul-04 19:12 0.042804 AU
6403314 km
6.00 km/s
2067-Jul-10 23:40 0.172632 AU
25825376 km
9.62 km/s
2068-Jul-16 06:20 0.304149 AU
45500016 km
13.41 km/s
2069-Jul-22 08:57 0.435944 AU
65216322 km
17.29 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
25.82

Orbit Quality

RMS
0.43179
Condition
1
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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