SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 DA54

2015 DA54

2015 DA54 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.604 AU it takes 4.20 yr to circle the Sun.

Apollo Observations: 70
Orbital Period · P
4.20 yr
v(q)
52.9 km/s
v(Q)
6.4 km/s
Diameter · ≈
0.24 km
TJ
2.87
Eccentricity · e
0.7827

Orbit and dynamics

Between its closest point (0.566 AU) and its farthest (4.642 AU), the heliocentric distance changes by 4.076 AU over every revolution.

One full revolution takes 4.20 yr (1,535 days), computed from the semi-major axis of 2.604 AU.

The high eccentricity (0.783) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.24° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 52.9 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

The measured diameter is 0.47 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.039 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

Astrometry from 70 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5107 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
2.604 AU
Eccentricity
0.7827
Perihelion
0.566 AU
Aphelion
4.642151 AU
Inclination
8.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
262.93°

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
2031-Oct-17 04:13 0.437050 AU
65381685 km
22.73 km/s
2036-Feb-13 00:17 0.395957 AU
59234371 km
35.37 km/s
2048-Jul-21 13:28 0.128733 AU
19258183 km
26.64 km/s
2053-Jan-07 09:49 0.198913 AU
29756912 km
17.24 km/s
2065-Jul-05 14:15 0.444760 AU
66535192 km
35.95 km/s
2069-Nov-22 19:49 0.393368 AU
58847044 km
20.04 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.468 km
Albedo
0.039
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.88

Orbit Quality

RMS
0.51072
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.