SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 EM89

2013 EM89

2013 EM89 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.178 AU once every 1.28 yr.

Amor Observations: 58
Orbital Period · P
1.28 yr
v(q)
30.8 km/s
v(Q)
24.4 km/s
Diameter · ≈
0.02 km
TJ
5.36
Eccentricity · e
0.1164

Orbit and dynamics

Between its closest point (1.041 AU) and its farthest (1.315 AU), the heliocentric distance changes by 0.274 AU over every revolution.

One full revolution takes 1.28 yr (467 days), computed from the semi-major axis of 1.178 AU.

An eccentricity of 0.116 makes the orbit moderately elongated.

Its inclination of 2.41° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 30.8 km/s at perihelion and falls to 24.4 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 = 26 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 58 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3777 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
1.178 AU
Eccentricity
0.1164
Perihelion
1.041 AU
Aphelion
1.315119 AU
Inclination
2.41°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
117.73°

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
2026-Dec-03 14:29 0.243785 AU
36469702 km
4.13 km/s
2027-Apr-24 00:35 0.374432 AU
56014178 km
11.93 km/s
2031-Sep-06 10:59 0.293894 AU
43965886 km
5.08 km/s
2036-Mar-26 09:45 0.044074 AU
6593305 km
2.31 km/s
2040-Oct-08 03:46 0.316489 AU
47346098 km
5.51 km/s
2045-Apr-03 10:57 0.135646 AU
20292427 km
4.20 km/s
2045-Jun-04 03:20 0.139041 AU
20800167 km
0.76 km/s
2049-Nov-07 02:19 0.293341 AU
43883210 km
5.06 km/s
2054-Aug-08 02:49 0.251697 AU
37653282 km
4.12 km/s
2058-Dec-18 02:10 0.210443 AU
31481868 km
3.50 km/s
2063-Sep-13 16:54 0.301908 AU
45164808 km
5.25 km/s
2068-Mar-28 23:09 0.019109 AU
2858619 km
1.93 km/s
2072-Oct-06 23:16 0.319441 AU
47787678 km
5.54 km/s
2077-Mar-31 18:44 0.057325 AU
8575676 km
2.97 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
26.0

Orbit Quality

RMS
0.37774
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.

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