SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 HO3

2019 HO3

2019 HO3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.038 AU it takes 1.06 yr to circle the Sun.

Apollo Observations: 104
Orbital Period · P
1.06 yr
v(q)
59.3 km/s
v(Q)
14.4 km/s
Diameter · ≈
0.07 km
TJ
5.72
Eccentricity · e
0.6087

Orbit and dynamics

The path is an ellipse reaching 0.406 AU from the Sun at perihelion and 1.67 AU at aphelion, a radial span of 1.264 AU.

Applying Kepler's third law to a = 1.038 AU gives an orbital period of 1.06 yr, or about 386 days.

The high eccentricity (0.609) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.25° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 59.3 km/s at perihelion and falls to 14.4 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 = 23.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.07 km.

Observation record and orbit quality

The current orbit solution is based on 104 observations and has a weighted RMS residual of 0.369 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
1.038 AU
Eccentricity
0.6087
Perihelion
0.406 AU
Aphelion
1.669831 AU
Inclination
3.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
204.89°

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-Jan-12 15:06 0.092278 AU
13804652 km
22.88 km/s
2028-Jan-27 14:02 0.418817 AU
62654096 km
33.94 km/s
2036-Apr-12 23:35 0.352641 AU
52754375 km
32.42 km/s
2037-Apr-27 07:55 0.016044 AU
2400080 km
21.86 km/s
2038-May-02 05:09 0.208819 AU
31238863 km
13.11 km/s
2044-Jan-14 16:02 0.324226 AU
48503445 km
12.63 km/s
2045-Jan-07 17:31 0.052964 AU
7923283 km
18.90 km/s
2046-Jan-21 15:01 0.289859 AU
43362355 km
29.78 km/s
2055-Apr-22 05:31 0.188412 AU
28185973 km
26.30 km/s
2056-May-03 02:02 0.095772 AU
14327328 km
16.16 km/s
2057-Apr-18 20:18 0.405841 AU
60712935 km
12.98 km/s
2057-Jun-25 22:49 0.452140 AU
67639248 km
14.61 km/s
2061-Nov-05 04:21 0.482617 AU
72198461 km
18.29 km/s
2062-Jan-24 21:29 0.453992 AU
67916309 km
13.42 km/s
2063-Jan-05 08:53 0.173651 AU
25977747 km
14.60 km/s
2064-Jan-15 18:41 0.171491 AU
25654693 km
24.91 km/s
2073-Apr-14 12:52 0.367329 AU
54951644 km
31.66 km/s
2074-Apr-28 15:40 0.030812 AU
4609431 km
21.19 km/s
2075-May-01 19:48 0.259693 AU
38849491 km
12.88 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
23.6

Orbit Quality

RMS
0.369
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

Explore asteroids, comets and near-Earth objects with JPL orbital data.