SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 YN10

2015 YN10

2015 YN10 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.087 AU it takes 1.13 yr to circle the Sun.

Apollo Observations: 82
Orbital Period · P
1.13 yr
v(q)
68.3 km/s
v(Q)
12 km/s
Diameter · ≈
0.28 km
TJ
5.38
Eccentricity · e
0.7016

Orbit and dynamics

Between its closest point (0.324 AU) and its farthest (1.85 AU), the heliocentric distance changes by 1.526 AU over every revolution.

One full revolution takes 1.13 yr (414 days), computed from the semi-major axis of 1.087 AU.

The high eccentricity (0.702) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 23.85° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 68.3 km/s at perihelion and falls to 12 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 = 20.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.28 km.

Observation record and orbit quality

Astrometry from 82 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6068 arcseconds.

Condition code U = 0 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
1.087 AU
Eccentricity
0.7016
Perihelion
0.324 AU
Aphelion
1.849639 AU
Inclination
23.85°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
156.17°

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
2029-Mar-17 07:23 0.331547 AU
49598745 km
26.40 km/s
2033-Dec-30 23:08 0.444594 AU
66510328 km
34.43 km/s
2038-Mar-20 11:36 0.441421 AU
66035600 km
17.78 km/s
2041-Dec-17 17:47 0.305222 AU
45660519 km
22.89 km/s
2046-Mar-18 05:25 0.328511 AU
49144500 km
25.91 km/s
2049-Dec-22 23:01 0.492568 AU
73687053 km
17.70 km/s
2051-Jan-01 00:29 0.455661 AU
68165958 km
34.92 km/s
2055-Mar-20 08:51 0.450254 AU
67357090 km
17.70 km/s
2058-Dec-18 11:34 0.302920 AU
45316151 km
23.34 km/s
2063-Mar-19 02:30 0.326394 AU
48827900 km
25.48 km/s
2066-Dec-22 16:18 0.482905 AU
72241622 km
17.70 km/s
2068-Jan-01 23:56 0.466186 AU
69740415 km
35.41 km/s
2072-Mar-19 04:54 0.459019 AU
68668326 km
17.62 km/s
2075-Dec-19 04:58 0.301427 AU
45092846 km
23.72 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
20.5

Orbit Quality

RMS
0.60681
Condition
0
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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