SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 DZ155

2015 DZ155

2015 DZ155 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.978 AU and a period of 0.97 yr.

Aten Observations: 30
Orbital Period · P
0.97 yr
v(q)
43 km/s
v(Q)
21.1 km/s
Diameter · ≈
0.05 km
TJ
6.11
Eccentricity · e
0.3409

Orbit and dynamics

The path is an ellipse reaching 0.644 AU from the Sun at perihelion and 1.311 AU at aphelion, a radial span of 0.667 AU.

Applying Kepler's third law to a = 0.978 AU gives an orbital period of 0.97 yr, or about 353 days.

An eccentricity of 0.341 makes the orbit moderately elongated.

The orbital plane is tilted 14.12° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43 km/s at perihelion and falls to 21.1 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 = 24.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

The current orbit solution is based on 30 observations and has a weighted RMS residual of 0.5285 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
0.9779 AU
Eccentricity
0.3409
Perihelion
0.644 AU
Aphelion
1.311266 AU
Inclination
14.12°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
164.39°

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-Oct-28 10:19 0.415510 AU
62159408 km
25.89 km/s
2036-Oct-17 07:20 0.248549 AU
37182413 km
19.91 km/s
2037-Oct-04 22:46 0.175703 AU
26284863 km
14.34 km/s
2044-Feb-22 03:34 0.046170 AU
6906902 km
10.79 km/s
2045-Feb-18 17:02 0.044961 AU
6726080 km
15.80 km/s
2046-Feb-11 18:26 0.238697 AU
35708556 km
21.75 km/s
2064-Oct-23 05:18 0.361648 AU
54101818 km
23.14 km/s
2065-Oct-12 03:25 0.206068 AU
30827333 km
17.16 km/s
2066-Sep-26 09:55 0.176598 AU
26418663 km
12.16 km/s
2072-Feb-18 00:45 0.088736 AU
13274668 km
9.62 km/s
2073-Feb-20 18:47 0.035853 AU
5363499 km
13.62 km/s
2074-Feb-14 12:22 0.127898 AU
19133236 km
19.58 km/s
2075-Feb-06 13:02 0.332266 AU
49706321 km
25.92 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
24.4

Orbit Quality

RMS
0.52852
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.

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