SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 AR3

2019 AR3

2019 AR3 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.867 AU and a period of 0.81 yr.

Aten Observations: 116
Orbital Period · P
0.81 yr
v(q)
62.6 km/s
v(Q)
16.4 km/s
Diameter · ≈
0.12 km
TJ
6.58
Eccentricity · e
0.5855

Orbit and dynamics

Between its closest point (0.359 AU) and its farthest (1.374 AU), the heliocentric distance changes by 1.015 AU over every revolution.

One full revolution takes 0.81 yr (295 days), computed from the semi-major axis of 0.867 AU.

The high eccentricity (0.586) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 29.65° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 62.6 km/s at perihelion and falls to 16.4 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 = 22.43 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

Astrometry from 116 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3768 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
0.8669 AU
Eccentricity
0.5855
Perihelion
0.359 AU
Aphelion
1.37447 AU
Inclination
29.65°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
151.45°

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-14 08:31 0.342605 AU
51253051 km
32.42 km/s
2028-Jan-28 00:17 0.486444 AU
72771038 km
17.30 km/s
2032-Jan-16 12:38 0.386551 AU
57827192 km
17.30 km/s
2036-Jan-06 16:31 0.238428 AU
35668288 km
17.52 km/s
2037-Apr-09 15:40 0.495394 AU
74109895 km
18.80 km/s
2040-Jan-02 04:56 0.067146 AU
10044914 km
19.52 km/s
2044-Jan-04 18:32 0.052783 AU
7896268 km
23.92 km/s
2048-Jan-11 07:09 0.192102 AU
28738091 km
29.69 km/s
2052-Jan-19 09:24 0.377287 AU
56441297 km
35.98 km/s
2053-Jan-20 19:10 0.407791 AU
61004633 km
17.31 km/s
2057-Jan-09 23:57 0.270379 AU
40448048 km
17.32 km/s
2058-Apr-01 22:17 0.495205 AU
74081593 km
20.70 km/s
2061-Jan-02 12:37 0.097209 AU
14542204 km
18.33 km/s
2065-Jan-02 09:05 0.051338 AU
7680121 km
21.82 km/s
2069-Jan-07 14:41 0.062428 AU
9339029 km
27.13 km/s
2073-Jan-15 05:39 0.216002 AU
32313425 km
33.32 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
22.43

Orbit Quality

RMS
0.3768
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.

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