SpaceAtlas Space Object Data
NASA JPL SBDB · 2014 CY4

2014 CY4

2014 CY4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.655 AU it takes 4.33 yr to circle the Sun.

Apollo Observations: 33
Orbital Period · P
4.33 yr
v(q)
57.9 km/s
v(Q)
5.8 km/s
Diameter · ≈
0.3 km
TJ
2.75
Eccentricity · e
0.8184

Orbit and dynamics

The path is an ellipse reaching 0.482 AU from the Sun at perihelion and 4.828 AU at aphelion, a radial span of 4.346 AU.

Applying Kepler's third law to a = 2.655 AU gives an orbital period of 4.33 yr, or about 1,580 days.

The high eccentricity (0.818) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 15.03° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 57.9 km/s at perihelion and falls to 5.8 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 0.57 km, a value from direct size determination rather than from brightness alone.

Its geometric albedo of 0.019 indicates a very dark, carbonaceous-type surface.

Observation record and orbit quality

The current orbit solution is based on 33 observations and has a weighted RMS residual of 0.4712 arcseconds.

Condition code U = 1 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
2.655 AU
Eccentricity
0.8184
Perihelion
0.482 AU
Aphelion
4.827852 AU
Inclination
15.03°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
320.74°

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
2052-Aug-22 02:53 0.280923 AU
42025538 km
19.08 km/s
2057-Mar-10 18:28 0.393643 AU
58888191 km
37.37 km/s
2065-Aug-12 10:55 0.120031 AU
17956396 km
23.86 km/s
2070-Mar-05 20:08 0.304445 AU
45544362 km
34.37 km/s
2078-Aug-11 06:24 0.104946 AU
15699709 km
24.57 km/s

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

Physical Parameters

Diameter
0.574 km
Albedo
0.019
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
20.34

Orbit Quality

RMS
0.47124
Condition
1
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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