SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 UL2

2019 UL2

2019 UL2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.241 AU it takes 1.38 yr to circle the Sun.

Apollo Observations: 49
Orbital Period · P
1.38 yr
v(q)
34.9 km/s
v(Q)
20.5 km/s
Diameter · ≈
0.04 km
TJ
5.13
Eccentricity · e
0.2595

Orbit and dynamics

The path is an ellipse reaching 0.919 AU from the Sun at perihelion and 1.563 AU at aphelion, a radial span of 0.644 AU.

Applying Kepler's third law to a = 1.241 AU gives an orbital period of 1.38 yr, or about 505 days.

An eccentricity of 0.26 makes the orbit moderately elongated.

Its inclination of 4.52° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.9 km/s at perihelion and falls to 20.5 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 = 24.84 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 49 observations and has a weighted RMS residual of 0.5848 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.241 AU
Eccentricity
0.2595
Perihelion
0.919 AU
Aphelion
1.56304 AU
Inclination
4.52°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
242.9°

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
2030-Sep-24 11:54 0.269807 AU
40362488 km
4.79 km/s
2031-Mar-01 19:06 0.053563 AU
8012952 km
7.66 km/s
2037-Oct-25 09:22 0.125200 AU
18729701 km
11.94 km/s
2038-Apr-28 15:14 0.345837 AU
51736512 km
6.28 km/s
2041-Aug-12 09:59 0.459212 AU
68697096 km
7.71 km/s
2042-Mar-24 19:45 0.401285 AU
60031358 km
20.14 km/s
2055-Oct-18 16:51 0.243290 AU
36395598 km
15.98 km/s
2056-May-11 06:13 0.402094 AU
60152441 km
7.15 km/s
2059-Aug-25 00:16 0.400854 AU
59966868 km
7.02 km/s
2060-Mar-17 05:31 0.239452 AU
35821558 km
15.87 km/s
2073-Oct-11 13:15 0.374360 AU
56003402 km
19.84 km/s
2074-May-22 13:40 0.450272 AU
67359683 km
7.76 km/s
2077-Sep-04 22:17 0.348634 AU
52154940 km
6.27 km/s
2078-Mar-11 11:22 0.130732 AU
19557212 km
12.37 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
24.84

Orbit Quality

RMS
0.58478
Condition
7
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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