SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 EK7

2015 EK7

2015 EK7 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.511 AU it takes 1.86 yr to circle the Sun.

Apollo Observations: 51
Orbital Period · P
1.86 yr
v(q)
35.6 km/s
v(Q)
16.5 km/s
Diameter · ≈
0.14 km
TJ
4.45
Eccentricity · e
0.3664

Orbit and dynamics

Between its closest point (0.957 AU) and its farthest (2.065 AU), the heliocentric distance changes by 1.108 AU over every revolution.

One full revolution takes 1.86 yr (678 days), computed from the semi-major axis of 1.511 AU.

An eccentricity of 0.366 makes the orbit moderately elongated.

Its inclination of 3.43° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.6 km/s at perihelion and falls to 16.5 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 = 21.99 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.14 km.

Observation record and orbit quality

Astrometry from 51 individual observations underpins this orbit; the fit leaves an RMS residual of 0.684 arcseconds.

Condition code U = 1 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
1.511 AU
Eccentricity
0.3664
Perihelion
0.957 AU
Aphelion
2.06463 AU
Inclination
3.43°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
319.59°

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
2028-Apr-01 18:51 0.429284 AU
64220039 km
3.73 km/s
2028-Aug-11 05:29 0.108176 AU
16182884 km
10.86 km/s
2041-Mar-23 09:20 0.480270 AU
71847341 km
5.31 km/s
2041-Aug-16 16:06 0.175576 AU
26265728 km
12.87 km/s
2043-Apr-08 08:57 0.427435 AU
63943372 km
20.12 km/s
2054-Aug-23 01:15 0.272397 AU
40749938 km
15.71 km/s
2056-Apr-12 20:34 0.330336 AU
49417629 km
17.22 km/s
2067-Aug-28 19:52 0.370866 AU
55480789 km
18.58 km/s
2069-Apr-18 20:08 0.234637 AU
35101215 km
14.31 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
21.99

Orbit Quality

RMS
0.68396
Condition
1
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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