SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 XW

2019 XW

2019 XW belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.273 AU it takes 1.44 yr to circle the Sun.

Apollo Observations: 104
Orbital Period · P
1.44 yr
v(q)
44.6 km/s
v(Q)
15.6 km/s
Diameter · ≈
0.06 km
TJ
4.95
Eccentricity · e
0.4804

Orbit and dynamics

The path is an ellipse reaching 0.661 AU from the Sun at perihelion and 1.885 AU at aphelion, a radial span of 1.224 AU.

Applying Kepler's third law to a = 1.273 AU gives an orbital period of 1.44 yr, or about 525 days.

The high eccentricity (0.48) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.85° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 44.6 km/s at perihelion and falls to 15.6 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 = 23.88 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 104 observations and has a weighted RMS residual of 0.3535 arcseconds.

Condition code U = 3 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
1.273 AU
Eccentricity
0.4804
Perihelion
0.661 AU
Aphelion
1.884549 AU
Inclination
7.85°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
151.28°

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-Jun-03 05:21 0.156129 AU
23356632 km
10.56 km/s
2030-Jan-20 21:29 0.268379 AU
40148933 km
10.63 km/s
2037-Jun-22 20:38 0.153725 AU
22996931 km
19.20 km/s
2040-Mar-12 07:03 0.350118 AU
52376851 km
14.58 km/s
2042-Dec-02 09:19 0.183322 AU
27424545 km
20.31 km/s
2047-Jul-10 01:17 0.490147 AU
73325012 km
29.15 km/s
2050-May-09 15:50 0.251363 AU
37603331 km
10.31 km/s
2052-Dec-27 08:12 0.192602 AU
28812841 km
9.39 km/s
2060-Jun-21 20:36 0.133636 AU
19991681 km
18.69 km/s
2063-Mar-14 21:40 0.349767 AU
52324450 km
14.60 km/s
2065-Dec-04 10:05 0.138614 AU
20736422 km
19.03 km/s
2073-May-31 11:23 0.170382 AU
25488741 km
10.18 km/s
2076-Jan-25 23:16 0.278709 AU
41694330 km
11.10 km/s
2078-Nov-19 19:10 0.459775 AU
68781343 km
28.65 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
23.88

Orbit Quality

RMS
0.35346
Condition
3
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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