SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 XD169

2015 XD169

2015 XD169 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.085 AU it takes 1.13 yr to circle the Sun.

Apollo Observations: 46
Orbital Period · P
1.13 yr
v(q)
32.3 km/s
v(Q)
25.3 km/s
Diameter · ≈
0.01 km
TJ
5.7
Eccentricity · e
0.1212

Orbit and dynamics

Between its closest point (0.954 AU) and its farthest (1.217 AU), the heliocentric distance changes by 0.263 AU over every revolution.

One full revolution takes 1.13 yr (413 days), computed from the semi-major axis of 1.085 AU.

An eccentricity of 0.121 makes the orbit moderately elongated.

Its inclination of 3.75° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.3 km/s at perihelion and falls to 25.3 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 = 26.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 46 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3676 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
1.085 AU
Eccentricity
0.1212
Perihelion
0.954 AU
Aphelion
1.216502 AU
Inclination
3.75°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
143.26°

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
2032-Aug-02 01:16 0.108154 AU
16179658 km
6.16 km/s
2033-Mar-02 14:21 0.195042 AU
29177829 km
3.84 km/s
2041-Jul-04 09:15 0.112033 AU
16759888 km
2.66 km/s
2041-Nov-08 02:48 0.042305 AU
6328798 km
2.85 km/s
2050-May-28 11:55 0.169313 AU
25328862 km
3.87 km/s
2050-Dec-12 04:43 0.052071 AU
7789753 km
5.44 km/s
2058-Jul-22 12:07 0.313828 AU
46947928 km
12.39 km/s
2059-Apr-12 20:27 0.219541 AU
32842797 km
4.56 km/s
2059-Dec-26 22:35 0.316811 AU
47394301 km
12.95 km/s
2067-Aug-04 04:55 0.092313 AU
13809851 km
5.16 km/s
2068-Feb-23 09:29 0.188540 AU
28205217 km
3.57 km/s
2076-Jul-06 12:13 0.109146 AU
16327995 km
2.56 km/s
2076-Nov-01 23:40 0.050112 AU
7496604 km
2.85 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
26.9

Orbit Quality

RMS
0.3676
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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