SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 ME116

2015 ME116

2015 ME116 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.036 AU it takes 1.05 yr to circle the Sun.

Apollo Observations: 67
Orbital Period · P
1.05 yr
v(q)
34 km/s
v(Q)
25.2 km/s
Diameter · ≈
0.12 km
TJ
5.83
Eccentricity · e
0.149

Orbit and dynamics

The path is an ellipse reaching 0.882 AU from the Sun at perihelion and 1.19 AU at aphelion, a radial span of 0.308 AU.

Applying Kepler's third law to a = 1.036 AU gives an orbital period of 1.05 yr, or about 385 days.

An eccentricity of 0.149 makes the orbit moderately elongated.

A steep inclination of 24.33° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34 km/s at perihelion and falls to 25.2 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 = 22.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

The current orbit solution is based on 67 observations and has a weighted RMS residual of 0.3765 arcseconds.

Condition code U = 2 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
1.036 AU
Eccentricity
0.149
Perihelion
0.882 AU
Aphelion
1.190364 AU
Inclination
24.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
351.91°

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
2033-Jul-27 20:55 0.276003 AU
41289422 km
16.15 km/s
2034-Jul-26 21:07 0.104472 AU
15628716 km
12.28 km/s
2035-Jan-03 07:56 0.274194 AU
41018875 km
14.14 km/s
2035-Jul-13 07:59 0.336608 AU
50355835 km
12.61 km/s
2036-Jan-27 19:06 0.086858 AU
12993779 km
14.34 km/s
2037-Feb-16 01:53 0.409909 AU
61321546 km
20.52 km/s
2052-Jul-26 22:35 0.329826 AU
49341203 km
17.30 km/s
2053-Jul-27 16:42 0.095241 AU
14247777 km
12.60 km/s
2053-Dec-28 15:03 0.330548 AU
49449275 km
14.76 km/s
2054-Jul-16 13:41 0.294123 AU
44000161 km
12.42 km/s
2055-Jan-23 22:49 0.055486 AU
8300613 km
13.79 km/s
2056-Feb-13 16:54 0.354725 AU
53066096 km
19.26 km/s
2071-Jul-26 23:57 0.370335 AU
55401268 km
18.23 km/s
2072-Jul-28 00:41 0.106200 AU
15887279 km
12.95 km/s
2072-Dec-23 11:32 0.374509 AU
56025736 km
15.30 km/s
2073-Jul-18 17:24 0.259836 AU
38870922 km
12.27 km/s
2074-Jan-20 16:58 0.065030 AU
9728363 km
13.50 km/s
2074-Jun-14 06:22 0.496002 AU
74200799 km
11.91 km/s
2075-Feb-10 17:44 0.306517 AU
45854290 km
18.22 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
22.3

Orbit Quality

RMS
0.37653
Condition
2
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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