SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 HU2

2017 HU2

2017 HU2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.869 AU and a period of 0.81 yr.

Aten Observations: 122
Orbital Period · P
0.81 yr
v(q)
37.7 km/s
v(Q)
27.1 km/s
Diameter · ≈
0.02 km
TJ
6.79
Eccentricity · e
0.1639

Orbit and dynamics

The path is an ellipse reaching 0.726 AU from the Sun at perihelion and 1.011 AU at aphelion, a radial span of 0.285 AU.

Applying Kepler's third law to a = 0.869 AU gives an orbital period of 0.81 yr, or about 296 days.

An eccentricity of 0.164 makes the orbit moderately elongated.

The orbital plane is tilted 6.23° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 37.7 km/s at perihelion and falls to 27.1 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 = 25.93 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 122 observations and has a weighted RMS residual of 0.3317 arcseconds.

Condition code U = 5 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
0.8687 AU
Eccentricity
0.1639
Perihelion
0.726 AU
Aphelion
1.01108 AU
Inclination
6.23°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
271.48°

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
2029-Dec-19 00:56 0.235077 AU
35167050 km
6.34 km/s
2030-May-18 22:22 0.210446 AU
31482332 km
9.50 km/s
2034-Apr-08 00:54 0.051134 AU
7649513 km
4.70 km/s
2038-Apr-06 15:27 0.400480 AU
59910901 km
15.38 km/s
2038-Oct-03 11:43 0.262169 AU
39219911 km
8.05 km/s
2042-Dec-03 08:58 0.248587 AU
37188014 km
7.39 km/s
2043-May-18 05:39 0.286819 AU
42907476 km
11.91 km/s
2047-Apr-12 22:53 0.027047 AU
4046177 km
4.28 km/s
2051-Apr-09 09:54 0.437368 AU
65429299 km
17.38 km/s
2051-Oct-16 09:37 0.261135 AU
39065284 km
8.31 km/s
2056-May-18 16:30 0.093699 AU
14017141 km
7.20 km/s
2060-Mar-31 22:34 0.157577 AU
23573151 km
9.69 km/s
2065-May-15 11:18 0.327286 AU
48961290 km
15.24 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
25.93

Orbit Quality

RMS
0.3317
Condition
5
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.