SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 UR5

2017 UR5

2017 UR5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.186 AU it takes 1.29 yr to circle the Sun.

Apollo Observations: 30
Orbital Period · P
1.29 yr
v(q)
33.8 km/s
v(Q)
22.1 km/s
Diameter · ≈
0.01 km
TJ
5.3
Eccentricity · e
0.2078

Orbit and dynamics

Between its closest point (0.94 AU) and its farthest (1.432 AU), the heliocentric distance changes by 0.492 AU over every revolution.

One full revolution takes 1.29 yr (472 days), computed from the semi-major axis of 1.186 AU.

An eccentricity of 0.208 makes the orbit moderately elongated.

The orbital plane is tilted 12.4° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 33.8 km/s at perihelion and falls to 22.1 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 = 28.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 30 individual observations underpins this orbit; the fit leaves an RMS residual of 0.436 arcseconds.

Condition code U = 6 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
1.186 AU
Eccentricity
0.2078
Perihelion
0.94 AU
Aphelion
1.432451 AU
Inclination
12.4°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
278.58°

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
2026-Nov-06 18:40 0.251067 AU
37559085 km
15.03 km/s
2030-Jun-04 23:55 0.256042 AU
38303395 km
12.47 km/s
2031-Jan-03 13:56 0.419649 AU
62778586 km
6.30 km/s
2035-Mar-19 16:20 0.445316 AU
66618286 km
8.86 km/s
2039-May-30 08:07 0.186930 AU
27964324 km
7.22 km/s
2044-Feb-26 02:39 0.486076 AU
72715933 km
8.61 km/s
2048-May-02 11:10 0.259061 AU
38755036 km
7.69 km/s
2048-Oct-24 15:18 0.010824 AU
1619318 km
9.28 km/s
2052-May-29 23:16 0.438507 AU
65599673 km
17.81 km/s
2053-Jan-27 16:34 0.477692 AU
71461721 km
7.51 km/s
2057-Mar-31 18:00 0.395846 AU
59217663 km
8.78 km/s
2057-Nov-13 02:19 0.314813 AU
47095338 km
18.68 km/s
2061-Jun-05 21:59 0.188316 AU
28171630 km
8.55 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
28.7

Orbit Quality

RMS
0.43605
Condition
6
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.