SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 QK

2019 QK

2019 QK belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.208 AU it takes 1.33 yr to circle the Sun.

Apollo Observations: 38
Orbital Period · P
1.33 yr
v(q)
71.8 km/s
v(Q)
10.2 km/s
Diameter · ≈
0.22 km
TJ
4.81
Eccentricity · e
0.7505

Orbit and dynamics

The path is an ellipse reaching 0.301 AU from the Sun at perihelion and 2.115 AU at aphelion, a radial span of 1.814 AU.

Applying Kepler's third law to a = 1.208 AU gives an orbital period of 1.33 yr, or about 485 days.

The high eccentricity (0.75) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 38.23° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 71.8 km/s at perihelion and falls to 10.2 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 = 21.01 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.22 km.

Observation record and orbit quality

The current orbit solution is based on 38 observations and has a weighted RMS residual of 0.4025 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
1.208 AU
Eccentricity
0.7505
Perihelion
0.301 AU
Aphelion
2.114604 AU
Inclination
38.23°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
83.53°

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-Aug-13 18:59 0.305712 AU
45733884 km
26.95 km/s
2031-Aug-12 07:45 0.312139 AU
46695339 km
25.15 km/s
2035-Aug-11 14:35 0.326105 AU
48784541 km
23.69 km/s
2039-Aug-11 17:30 0.349712 AU
52316192 km
22.57 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
21.01

Orbit Quality

RMS
0.40246
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.

Keep exploring

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