SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 UT6

2019 UT6

2019 UT6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.59 AU it takes 2.00 yr to circle the Sun.

Apollo Observations: 368
Orbital Period · P
2.00 yr
v(q)
41.2 km/s
v(Q)
13.6 km/s
Diameter · ≈
0.15 km
TJ
4.23
Eccentricity · e
0.5047

Orbit and dynamics

The path is an ellipse reaching 0.787 AU from the Sun at perihelion and 2.392 AU at aphelion, a radial span of 1.605 AU.

Applying Kepler's third law to a = 1.59 AU gives an orbital period of 2.00 yr, or about 732 days.

The high eccentricity (0.505) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.44° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 41.2 km/s at perihelion and falls to 13.6 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 = 21.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.15 km.

Observation record and orbit quality

The current orbit solution is based on 368 observations and has a weighted RMS residual of 0.3822 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
1.59 AU
Eccentricity
0.5047
Perihelion
0.787 AU
Aphelion
2.392473 AU
Inclination
2.44°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
74.04°

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-Nov-28 19:23 0.033987 AU
5084353 km
11.79 km/s
2029-Dec-03 18:01 0.073028 AU
10924901 km
10.64 km/s
2031-Dec-12 08:37 0.113141 AU
16925672 km
9.81 km/s
2033-Dec-25 02:44 0.152505 AU
22814421 km
9.82 km/s
2036-Jan-06 05:24 0.176153 AU
26352103 km
10.32 km/s
2038-Jan-17 08:37 0.192206 AU
28753619 km
10.80 km/s
2040-Jan-30 09:24 0.198867 AU
29750087 km
11.00 km/s
2042-Feb-11 00:22 0.195073 AU
29182550 km
10.80 km/s
2044-Feb-24 02:40 0.181858 AU
27205566 km
10.31 km/s
2046-Mar-11 02:52 0.151508 AU
22665207 km
9.64 km/s
2048-Mar-23 14:18 0.112066 AU
16764794 km
9.84 km/s
2050-Apr-01 23:42 0.068216 AU
10204965 km
11.04 km/s
2052-Apr-06 21:01 0.039877 AU
5965473 km
12.45 km/s
2054-Apr-11 07:29 0.055565 AU
8312473 km
13.84 km/s
2056-Apr-15 01:47 0.105668 AU
15807693 km
15.61 km/s
2058-Apr-20 03:47 0.177907 AU
26614505 km
17.82 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
21.9

Orbit Quality

RMS
0.38218
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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