SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 EJ55

2016 EJ55

2016 EJ55 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.164 AU it takes 1.26 yr to circle the Sun.

Apollo Observations: 67
Orbital Period · P
1.26 yr
v(q)
35.7 km/s
v(Q)
21.4 km/s
Diameter · ≈
0.04 km
TJ
5.38
Eccentricity · e
0.2509

Orbit and dynamics

Between its closest point (0.872 AU) and its farthest (1.456 AU), the heliocentric distance changes by 0.584 AU over every revolution.

One full revolution takes 1.26 yr (459 days), computed from the semi-major axis of 1.164 AU.

An eccentricity of 0.251 makes the orbit moderately elongated.

The orbital plane is tilted 7.2° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.7 km/s at perihelion and falls to 21.4 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 = 24.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 67 individual observations underpins this orbit; the fit leaves an RMS residual of 0.2893 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.164 AU
Eccentricity
0.2509
Perihelion
0.872 AU
Aphelion
1.456048 AU
Inclination
7.2°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
115.13°

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
2030-Jul-07 18:44 0.429716 AU
64284543 km
7.83 km/s
2031-Mar-17 12:16 0.274163 AU
41014154 km
18.00 km/s
2044-Sep-17 17:30 0.210075 AU
31426748 km
17.53 km/s
2049-Sep-24 17:41 0.072609 AU
10862184 km
13.33 km/s
2054-Oct-01 05:41 0.064274 AU
9615253 km
9.44 km/s
2059-Oct-06 14:57 0.064655 AU
9672198 km
6.34 km/s
2079-Aug-08 22:44 0.337068 AU
50424690 km
6.75 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
24.6

Orbit Quality

RMS
0.2893
Condition
7
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

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