SpaceAtlas Space Object Data
NASA JPL SBDB · 2013 ER89

2013 ER89

2013 ER89 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.695 AU it takes 2.21 yr to circle the Sun.

Apollo Observations: 125
Orbital Period · P
2.21 yr
v(q)
41.6 km/s
v(Q)
12.6 km/s
Diameter · ≈
0.32 km
TJ
3.93
Eccentricity · e
0.5358

Orbit and dynamics

The path is an ellipse reaching 0.787 AU from the Sun at perihelion and 2.603 AU at aphelion, a radial span of 1.816 AU.

Applying Kepler's third law to a = 1.695 AU gives an orbital period of 2.21 yr, or about 806 days.

The high eccentricity (0.536) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 26.99° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 41.6 km/s at perihelion and falls to 12.6 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 = 20.21 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.32 km.

Observation record and orbit quality

The current orbit solution is based on 125 observations and has a weighted RMS residual of 0.543 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
1.695 AU
Eccentricity
0.5358
Perihelion
0.787 AU
Aphelion
2.603181 AU
Inclination
26.99°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
317.41°

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
2035-Aug-29 16:18 0.367769 AU
55017387 km
14.47 km/s
2046-Sep-12 22:31 0.159505 AU
23861645 km
17.33 km/s
2055-Mar-29 08:51 0.424241 AU
63465570 km
28.52 km/s
2057-Sep-22 02:17 0.062849 AU
9402062 km
21.17 km/s
2066-Apr-05 20:40 0.267688 AU
40045559 km
23.15 km/s
2068-Oct-01 23:16 0.268446 AU
40158880 km
26.40 km/s
2077-Apr-12 00:30 0.232616 AU
34798898 km
18.24 km/s
2079-Oct-12 19:24 0.487854 AU
72981894 km
32.13 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
20.21

Orbit Quality

RMS
0.543
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.

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