SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 DZ53

2015 DZ53

2015 DZ53 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.512 AU it takes 1.86 yr to circle the Sun.

Apollo Observations: 63
Orbital Period · P
1.86 yr
v(q)
92 km/s
v(Q)
6.4 km/s
Diameter · ≈
0.23 km
TJ
3.97
Eccentricity · e
0.8705

Orbit and dynamics

Between its closest point (0.196 AU) and its farthest (2.828 AU), the heliocentric distance changes by 2.632 AU over every revolution.

One full revolution takes 1.86 yr (679 days), computed from the semi-major axis of 1.512 AU.

The high eccentricity (0.871) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.32° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 92 km/s at perihelion and falls to 6.4 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 = 20.94 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.23 km.

Observation record and orbit quality

Astrometry from 63 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6123 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
1.512 AU
Eccentricity
0.8705
Perihelion
0.196 AU
Aphelion
2.828196 AU
Inclination
8.32°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
356.66°

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-Mar-15 09:46 0.148483 AU
22212703 km
30.23 km/s
2033-Dec-26 09:56 0.259608 AU
38836812 km
40.34 km/s
2041-Mar-20 06:48 0.229810 AU
34379024 km
26.83 km/s
2047-Jan-01 23:33 0.389147 AU
58215569 km
44.83 km/s
2048-Dec-02 14:33 0.434757 AU
65038742 km
21.09 km/s
2054-Mar-25 14:51 0.379463 AU
56766865 km
22.51 km/s
2056-Feb-21 09:04 0.456296 AU
68260961 km
46.78 km/s
2061-Dec-06 07:45 0.270587 AU
40479294 km
24.91 km/s
2069-Feb-27 18:42 0.320871 AU
48001591 km
41.79 km/s
2074-Dec-11 18:14 0.129463 AU
19367424 km
29.10 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
20.94

Orbit Quality

RMS
0.61235
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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