SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 MS59

2015 MS59

2015 MS59 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.188 AU once every 3.24 yr.

Amor Observations: 184
Orbital Period · P
3.24 yr
v(q)
31.4 km/s
v(Q)
12.9 km/s
Diameter · ≈
0.22 km
TJ
3.55
Eccentricity · e
0.4184

Orbit and dynamics

The path is an ellipse reaching 1.273 AU from the Sun at perihelion and 3.103 AU at aphelion, a radial span of 1.83 AU.

Applying Kepler's third law to a = 2.188 AU gives an orbital period of 3.24 yr, or about 1,182 days.

The high eccentricity (0.418) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.87° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 31.4 km/s at perihelion and falls to 12.9 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 21 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

The current orbit solution is based on 184 observations and has a weighted RMS residual of 0.3437 arcseconds.

Condition code U = 4 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
2.188 AU
Eccentricity
0.4184
Perihelion
1.273 AU
Aphelion
3.103459 AU
Inclination
2.87°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
118.35°

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-Sep-21 05:31 0.404760 AU
60551295 km
1.81 km/s
2057-Aug-16 15:21 0.318927 AU
47710824 km
2.42 km/s
2070-Sep-11 04:42 0.316117 AU
47290398 km
2.45 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
21.0

Orbit Quality

RMS
0.34373
Condition
4
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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