SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 YM10

2015 YM10

2015 YM10 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.515 AU it takes 3.99 yr to circle the Sun.

Apollo Observations: 71
Orbital Period · P
3.99 yr
v(q)
78.1 km/s
v(Q)
4.5 km/s
Diameter · ≈
0.38 km
TJ
2.67
Eccentricity · e
0.8906

Orbit and dynamics

The path is an ellipse reaching 0.275 AU from the Sun at perihelion and 4.755 AU at aphelion, a radial span of 4.48 AU.

Applying Kepler's third law to a = 2.515 AU gives an orbital period of 3.99 yr, or about 1,457 days.

The high eccentricity (0.891) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 18.6° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 78.1 km/s at perihelion and falls to 4.5 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 = 19.83 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.38 km.

Observation record and orbit quality

The current orbit solution is based on 71 observations and has a weighted RMS residual of 0.6541 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
2.515 AU
Eccentricity
0.8906
Perihelion
0.275 AU
Aphelion
4.754859 AU
Inclination
18.6°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
204.66°

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
2028-Jan-21 02:19 0.287134 AU
42954700 km
35.13 km/s
2032-Jan-19 12:54 0.297032 AU
44435404 km
36.13 km/s
2036-Jan-16 12:30 0.326647 AU
48865766 km
38.19 km/s
2040-Jan-15 08:27 0.344903 AU
51596699 km
39.14 km/s
2044-Jan-15 20:09 0.338551 AU
50646534 km
38.81 km/s
2048-Jan-15 01:54 0.348798 AU
52179487 km
39.36 km/s
2052-Jan-15 10:53 0.347827 AU
52034181 km
39.23 km/s
2056-Jan-17 10:59 0.324194 AU
48498790 km
37.93 km/s
2060-Jan-17 22:51 0.318686 AU
47674759 km
37.60 km/s
2064-Jan-19 04:01 0.309127 AU
46244719 km
36.92 km/s
2068-Jan-21 17:21 0.289241 AU
43269771 km
35.25 km/s
2072-Jan-22 18:08 0.283358 AU
42389727 km
34.56 km/s
2076-Jan-23 16:06 0.280252 AU
41925055 km
34.03 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
19.83

Orbit Quality

RMS
0.65411
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.

Keep exploring

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