SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 HP3

2019 HP3

2019 HP3 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.962 AU and a period of 0.94 yr.

Aten Observations: 73
Orbital Period · P
0.94 yr
v(q)
33.1 km/s
v(Q)
27.9 km/s
Diameter · ≈
0.03 km
TJ
6.25
Eccentricity · e
0.0843

Orbit and dynamics

The path is an ellipse reaching 0.88 AU from the Sun at perihelion and 1.043 AU at aphelion, a radial span of 0.163 AU.

Applying Kepler's third law to a = 0.962 AU gives an orbital period of 0.94 yr, or about 344 days.

With e = 0.084, the orbit is close to circular.

The orbital plane is tilted 10.96° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.1 km/s at perihelion and falls to 27.9 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 = 25.68 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 73 observations and has a weighted RMS residual of 0.4399 arcseconds.

Condition code U = 4 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
0.9615 AU
Eccentricity
0.0843
Perihelion
0.88 AU
Aphelion
1.042554 AU
Inclination
10.96°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
21.52°

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
2034-Mar-15 13:30 0.462185 AU
69141884 km
15.20 km/s
2035-Apr-08 21:18 0.153483 AU
22960770 km
6.82 km/s
2035-Oct-16 08:03 0.127130 AU
19018359 km
6.73 km/s
2036-May-11 18:48 0.154545 AU
23119667 km
7.73 km/s
2037-May-16 00:09 0.479611 AU
71748825 km
16.52 km/s
2051-Mar-20 14:46 0.302533 AU
45258361 km
10.26 km/s
2051-Nov-20 18:27 0.122491 AU
18324323 km
6.76 km/s
2052-Apr-28 06:51 0.035845 AU
5362405 km
5.78 km/s
2052-Aug-24 21:30 0.196891 AU
29454452 km
5.06 km/s
2053-May-16 18:23 0.314637 AU
47068995 km
11.83 km/s
2067-Mar-14 13:46 0.452916 AU
67755222 km
15.37 km/s
2068-Apr-06 21:09 0.146171 AU
21866916 km
6.91 km/s
2068-Oct-16 14:04 0.122080 AU
18262907 km
6.73 km/s
2069-May-11 10:54 0.132283 AU
19789304 km
7.59 km/s
2070-May-15 23:01 0.455626 AU
68160606 km
16.30 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
25.68

Orbit Quality

RMS
0.4399
Condition
4
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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