SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 DS53

2015 DS53

2015 DS53 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.146 AU it takes 1.23 yr to circle the Sun.

Apollo Observations: 74
Orbital Period · P
1.23 yr
v(q)
44.9 km/s
v(Q)
17.2 km/s
Diameter · ≈
0.05 km
TJ
5.38
Eccentricity · e
0.4452

Orbit and dynamics

The path is an ellipse reaching 0.636 AU from the Sun at perihelion and 1.656 AU at aphelion, a radial span of 1.02 AU.

Applying Kepler's third law to a = 1.146 AU gives an orbital period of 1.23 yr, or about 448 days.

The high eccentricity (0.445) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.35° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.9 km/s at perihelion and falls to 17.2 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 = 24.2 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 74 observations and has a weighted RMS residual of 0.5144 arcseconds.

Condition code U = 3 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.146 AU
Eccentricity
0.4452
Perihelion
0.636 AU
Aphelion
1.656199 AU
Inclination
4.35°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
19.96°

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
2027-Oct-03 14:21 0.188582 AU
28211399 km
19.89 km/s
2031-Feb-15 19:54 0.337577 AU
50500736 km
24.58 km/s
2032-Jul-28 13:08 0.324201 AU
48499789 km
12.14 km/s
2032-Oct-09 22:16 0.374929 AU
56088518 km
8.44 km/s
2037-Feb-02 14:55 0.450161 AU
67343056 km
9.89 km/s
2037-May-16 01:19 0.360164 AU
53879805 km
14.18 km/s
2038-Oct-15 01:34 0.445145 AU
66592780 km
27.76 km/s
2042-Feb-27 12:39 0.070423 AU
10535200 km
16.40 km/s
2043-Sep-19 01:03 0.122567 AU
18335767 km
10.76 km/s
2048-Jun-15 03:58 0.384917 AU
57582738 km
15.58 km/s
2053-Mar-10 05:25 0.152341 AU
22789818 km
9.83 km/s
2054-Sep-29 13:29 0.099893 AU
14943741 km
17.21 km/s
2058-Feb-11 20:15 0.426055 AU
63736984 km
27.32 km/s
2059-Jul-16 03:25 0.353887 AU
52940711 km
13.73 km/s
2059-Oct-20 14:48 0.436470 AU
65295036 km
9.48 km/s
2064-Feb-12 13:19 0.390013 AU
58345045 km
8.92 km/s
2064-May-02 17:30 0.332887 AU
49799219 km
12.70 km/s
2065-Oct-10 20:39 0.353237 AU
52843460 km
24.92 km/s
2069-Feb-23 02:13 0.170569 AU
25516814 km
19.43 km/s
2070-Sep-07 17:10 0.219356 AU
32815125 km
8.14 km/s
2075-Jun-05 02:30 0.382057 AU
57154895 km
15.45 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
24.2

Orbit Quality

RMS
0.51441
Condition
3
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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