SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 YX7

2015 YX7

2015 YX7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.457 AU it takes 3.85 yr to circle the Sun.

Apollo Observations: 73
Orbital Period · P
3.85 yr
v(q)
38.3 km/s
v(Q)
9.4 km/s
Diameter · ≈
0.15 km
TJ
3.21
Eccentricity · e
0.6049

Orbit and dynamics

Between its closest point (0.971 AU) and its farthest (3.943 AU), the heliocentric distance changes by 2.972 AU over every revolution.

One full revolution takes 3.85 yr (1,407 days), computed from the semi-major axis of 2.457 AU.

The high eccentricity (0.605) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.03° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.3 km/s at perihelion and falls to 9.4 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

The measured diameter is 0.11 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.23 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 73 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5064 arcseconds.

Condition code U = 5 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
2.457 AU
Eccentricity
0.6049
Perihelion
0.971 AU
Aphelion
3.943239 AU
Inclination
4.03°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
266.79°

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
2039-Jan-15 14:44 0.374954 AU
56092365 km
21.61 km/s
2042-Sep-12 08:24 0.374308 AU
55995745 km
21.87 km/s
2062-Jan-14 22:22 0.335343 AU
50166542 km
21.05 km/s
2065-Sep-08 22:03 0.414392 AU
61992113 km
23.39 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.11 km
Albedo
0.23
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
21.82

Orbit Quality

RMS
0.5064
Condition
5
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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