SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 XM69

2010 XM69

2010 XM69 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.128 AU it takes 1.20 yr to circle the Sun.

Apollo Observations: 116
Orbital Period · P
1.20 yr
v(q)
57.1 km/s
v(Q)
13.8 km/s
Diameter · ≈
0.45 km
TJ
5.14
Eccentricity · e
0.6115

Orbit and dynamics

Between its closest point (0.438 AU) and its farthest (1.818 AU), the heliocentric distance changes by 1.38 AU over every revolution.

One full revolution takes 1.20 yr (438 days), computed from the semi-major axis of 1.128 AU.

The high eccentricity (0.612) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 44.1° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 57.1 km/s at perihelion and falls to 13.8 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 = 19.49 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.45 km.

Observation record and orbit quality

Astrometry from 116 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5232 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
1.128 AU
Eccentricity
0.6115
Perihelion
0.438 AU
Aphelion
1.817772 AU
Inclination
44.1°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
76.95°

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
2041-Nov-24 06:43 0.461159 AU
68988386 km
35.49 km/s
2047-Nov-22 15:08 0.415199 AU
62112902 km
33.74 km/s
2053-Nov-20 02:33 0.372907 AU
55786063 km
32.03 km/s
2059-Nov-18 19:39 0.337827 AU
50538244 km
30.42 km/s
2065-Nov-16 19:44 0.311944 AU
46666212 km
28.97 km/s
2071-Nov-16 02:48 0.296351 AU
44333471 km
27.69 km/s
2077-Nov-14 15:28 0.291304 AU
43578406 km
26.49 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
19.49

Orbit Quality

RMS
0.52318
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.

Keep exploring

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