SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 RR2

2019 RR2

2019 RR2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.014 AU it takes 1.02 yr to circle the Sun.

Apollo Observations: 14
Orbital Period · P
1.02 yr
v(q)
34.1 km/s
v(Q)
25.7 km/s
Diameter · ≈
0.02 km
TJ
6
Eccentricity · e
0.1411

Orbit and dynamics

The path is an ellipse reaching 0.871 AU from the Sun at perihelion and 1.157 AU at aphelion, a radial span of 0.286 AU.

Applying Kepler's third law to a = 1.014 AU gives an orbital period of 1.02 yr, or about 373 days.

An eccentricity of 0.141 makes the orbit moderately elongated.

The orbital plane is tilted 7.89° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34.1 km/s at perihelion and falls to 25.7 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 = 26.6 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 14 observations and has a weighted RMS residual of 0.3452 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
1.014 AU
Eccentricity
0.1411
Perihelion
0.871 AU
Aphelion
1.157075 AU
Inclination
7.89°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
310.64°

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
2060-Feb-04 20:54 0.351769 AU
52623914 km
17.79 km/s
2061-Feb-09 18:22 0.219527 AU
32840785 km
13.94 km/s
2062-Feb-15 23:18 0.088521 AU
13242608 km
10.20 km/s
2063-Feb-22 17:04 0.015745 AU
2355360 km
6.86 km/s
2064-Mar-03 23:28 0.051372 AU
7685144 km
4.73 km/s
2065-Jan-10 14:02 0.187240 AU
28010714 km
4.13 km/s
2065-Apr-21 16:11 0.165127 AU
24702721 km
4.77 km/s
2065-Nov-29 19:06 0.219701 AU
32866800 km
4.47 km/s
2066-Jun-06 14:07 0.186702 AU
27930150 km
4.62 km/s
2068-Aug-30 12:35 0.006547 AU
979454 km
5.74 km/s
2069-Sep-02 06:15 0.044000 AU
6582265 km
7.80 km/s
2070-Sep-05 23:54 0.131858 AU
19725749 km
10.37 km/s
2071-Sep-10 05:34 0.168671 AU
25232762 km
13.14 km/s
2072-Sep-13 10:58 0.208460 AU
31185098 km
16.03 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
26.6

Orbit Quality

RMS
0.34518
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.

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