SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 DC200

2015 DC200

2015 DC200 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.776 AU it takes 2.37 yr to circle the Sun.

Apollo Observations: 138
Orbital Period · P
2.37 yr
v(q)
83.6 km/s
v(Q)
6 km/s
Diameter · ≈
0.26 km
TJ
3.51
Eccentricity · e
0.8665

Orbit and dynamics

The path is an ellipse reaching 0.237 AU from the Sun at perihelion and 3.315 AU at aphelion, a radial span of 3.078 AU.

Applying Kepler's third law to a = 1.776 AU gives an orbital period of 2.37 yr, or about 864 days.

The high eccentricity (0.867) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.05° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 83.6 km/s at perihelion and falls to 6 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 = 20.66 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.26 km.

Observation record and orbit quality

The current orbit solution is based on 138 observations and has a weighted RMS residual of 0.5207 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
1.776 AU
Eccentricity
0.8665
Perihelion
0.237 AU
Aphelion
3.314904 AU
Inclination
3.05°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
239.52°

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
2034-Mar-20 04:31 0.042704 AU
6388396 km
32.58 km/s
2050-Dec-19 22:06 0.179569 AU
26863070 km
37.44 km/s
2060-Mar-17 11:25 0.081573 AU
12203198 km
34.19 km/s
2076-Dec-10 05:54 0.055236 AU
8263244 km
30.65 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
20.66

Orbit Quality

RMS
0.52069
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

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