SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 WN2

2019 WN2

2019 WN2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.288 AU it takes 1.46 yr to circle the Sun.

Apollo Observations: 30
Orbital Period · P
1.46 yr
v(q)
32.9 km/s
v(Q)
20.9 km/s
Diameter · ≈
0.01 km
TJ
5.01
Eccentricity · e
0.2221

Orbit and dynamics

The path is an ellipse reaching 1.002 AU from the Sun at perihelion and 1.574 AU at aphelion, a radial span of 0.572 AU.

Applying Kepler's third law to a = 1.288 AU gives an orbital period of 1.46 yr, or about 534 days.

An eccentricity of 0.222 makes the orbit moderately elongated.

Its inclination of 2° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.9 km/s at perihelion and falls to 20.9 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 27.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 30 observations and has a weighted RMS residual of 0.6953 arcseconds.

Condition code U = 5 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
1.288 AU
Eccentricity
0.2221
Perihelion
1.002 AU
Aphelion
1.574065 AU
Inclination
2.0°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
163.91°

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
2035-Aug-15 17:38 0.379364 AU
56751972 km
5.31 km/s
2036-Jan-26 12:12 0.439564 AU
65757889 km
16.23 km/s
2038-Nov-20 06:12 0.021187 AU
3169522 km
3.24 km/s
2042-Apr-09 21:30 0.433063 AU
64785358 km
6.62 km/s
2051-Aug-19 10:59 0.361339 AU
54055525 km
5.03 km/s
2052-Jan-26 00:49 0.402725 AU
60246813 km
15.15 km/s
2054-Oct-27 01:46 0.162858 AU
24363196 km
7.90 km/s
2055-Feb-11 06:03 0.231401 AU
34617141 km
1.71 km/s
2058-Apr-24 21:28 0.481454 AU
72024522 km
7.43 km/s
2064-Jul-16 16:56 0.477255 AU
71396340 km
7.20 km/s
2068-Jan-09 20:01 0.132980 AU
19893481 km
7.24 km/s
2070-Oct-10 21:15 0.404449 AU
60504650 km
15.56 km/s
2071-Mar-24 14:13 0.362903 AU
54289549 km
5.44 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
27.6

Orbit Quality

RMS
0.69528
Condition
5
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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