SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 AZ3

2017 AZ3

2017 AZ3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.297 AU it takes 1.48 yr to circle the Sun.

Apollo Observations: 34
Orbital Period · P
1.48 yr
v(q)
34.5 km/s
v(Q)
19.8 km/s
TJ
4.97
Eccentricity · e
0.2704

Orbit and dynamics

The path is an ellipse reaching 0.946 AU from the Sun at perihelion and 1.648 AU at aphelion, a radial span of 0.702 AU.

Applying Kepler's third law to a = 1.297 AU gives an orbital period of 1.48 yr, or about 540 days.

An eccentricity of 0.27 makes the orbit moderately elongated.

Its inclination of 4.03° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.5 km/s at perihelion and falls to 19.8 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2017 AZ3, so its physical size remains unconstrained.

Observation record and orbit quality

The current orbit solution is based on 34 observations and has a weighted RMS residual of 0.5304 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
1.297 AU
Eccentricity
0.2704
Perihelion
0.946 AU
Aphelion
1.647709 AU
Inclination
4.03°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
115.67°

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
2041-Oct-12 14:57 0.450653 AU
67416709 km
7.34 km/s
2042-Apr-29 17:33 0.359910 AU
53841763 km
18.61 km/s
2045-Apr-12 07:47 0.089065 AU
13323879 km
10.01 km/s
2050-Dec-19 00:45 0.141606 AU
21183999 km
11.34 km/s
2051-May-26 18:29 0.337385 AU
50472121 km
5.20 km/s
2053-Dec-04 02:33 0.454705 AU
68022917 km
19.39 km/s
2054-Jun-20 16:03 0.480213 AU
71838860 km
7.39 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
30.0

Orbit Quality

RMS
0.53038
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.