SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 CM

2015 CM

2015 CM belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.049 AU it takes 1.07 yr to circle the Sun.

Apollo Observations: 73
Orbital Period · P
1.07 yr
v(q)
30.3 km/s
v(Q)
27.9 km/s
Diameter · ≈
0.02 km
TJ
5.84
Eccentricity · e
0.0415

Orbit and dynamics

The path is an ellipse reaching 1.006 AU from the Sun at perihelion and 1.093 AU at aphelion, a radial span of 0.087 AU.

Applying Kepler's third law to a = 1.049 AU gives an orbital period of 1.07 yr, or about 392 days.

With e = 0.042, the orbit is close to circular.

The orbital plane is tilted 11.38° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 30.3 km/s at perihelion and falls to 27.9 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 73 observations and has a weighted RMS residual of 0.4694 arcseconds.

Condition code U = 6 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
1.049 AU
Eccentricity
0.0415
Perihelion
1.006 AU
Aphelion
1.092534 AU
Inclination
11.38°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
216.76°

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-Feb-10 05:45 0.188494 AU
28198353 km
8.29 km/s
2029-Aug-07 10:50 0.081899 AU
12251876 km
5.91 km/s
2030-Feb-09 19:19 0.237429 AU
35518849 km
9.73 km/s
2043-Feb-18 22:46 0.359933 AU
53845224 km
12.22 km/s
2043-Aug-27 23:47 0.111322 AU
16653517 km
6.33 km/s
2044-Feb-09 12:58 0.043445 AU
6499310 km
6.39 km/s
2057-Sep-10 20:17 0.205721 AU
30775367 km
7.18 km/s
2058-Feb-08 20:31 0.037826 AU
5658723 km
6.06 km/s
2058-Jul-16 21:51 0.188611 AU
28215783 km
6.65 km/s
2059-Feb-11 02:18 0.414969 AU
62078513 km
13.82 km/s
2072-Feb-13 08:50 0.274336 AU
41040116 km
10.36 km/s
2072-Aug-17 22:30 0.079400 AU
11878062 km
5.93 km/s
2073-Feb-09 01:59 0.121273 AU
18142139 km
7.56 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
26.1

Orbit Quality

RMS
0.46938
Condition
6
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.