SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 YK2

2018 YK2

2018 YK2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.529 AU it takes 4.02 yr to circle the Sun.

Apollo Observations: 221
Orbital Period · P
4.02 yr
v(q)
41.2 km/s
v(Q)
8.5 km/s
Diameter · ≈
0.1 km
TJ
3.1
Eccentricity · e
0.658

Orbit and dynamics

Between its closest point (0.865 AU) and its farthest (4.193 AU), the heliocentric distance changes by 3.328 AU over every revolution.

One full revolution takes 4.02 yr (1,469 days), computed from the semi-major axis of 2.529 AU.

The high eccentricity (0.658) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.06° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41.2 km/s at perihelion and falls to 8.5 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 = 22.79 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

Astrometry from 221 individual observations underpins this orbit; the fit leaves an RMS residual of 0.2996 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
2.529 AU
Eccentricity
0.658
Perihelion
0.865 AU
Aphelion
4.193082 AU
Inclination
7.06°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
317.39°

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-Jan-04 20:02 0.168372 AU
25188032 km
18.86 km/s
2031-Jan-12 19:15 0.277431 AU
41503138 km
22.41 km/s
2035-Jan-16 02:55 0.333676 AU
49917173 km
24.15 km/s
2039-Jan-20 22:46 0.428241 AU
64063959 km
26.87 km/s
2043-Jan-25 00:57 0.475970 AU
71204029 km
28.68 km/s
2047-Jan-23 19:03 0.447684 AU
66972576 km
27.90 km/s
2051-Jan-23 17:31 0.450753 AU
67431687 km
27.92 km/s
2055-Jan-23 08:55 0.409654 AU
61283369 km
27.11 km/s
2059-Jan-16 08:30 0.274762 AU
41103739 km
23.18 km/s
2063-Jan-10 00:47 0.173241 AU
25916455 km
20.08 km/s
2067-Jan-02 14:58 0.049457 AU
7398617 km
16.65 km/s
2070-Dec-08 15:05 0.131099 AU
19612082 km
12.78 km/s
2074-Nov-04 03:52 0.193240 AU
28908225 km
13.07 km/s
2078-Sep-29 07:30 0.175490 AU
26252957 km
12.67 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
22.79

Orbit Quality

RMS
0.2996
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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