SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 RP2

2019 RP2

2019 RP2 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 1.154 AU once every 1.24 yr.

Amor Observations: 25
Orbital Period · P
1.24 yr
v(q)
31.1 km/s
v(Q)
24.7 km/s
Diameter · ≈
0.01 km
TJ
5.45
Eccentricity · e
0.1136

Orbit and dynamics

The path is an ellipse reaching 1.023 AU from the Sun at perihelion and 1.285 AU at aphelion, a radial span of 0.262 AU.

Applying Kepler's third law to a = 1.154 AU gives an orbital period of 1.24 yr, or about 453 days.

An eccentricity of 0.114 makes the orbit moderately elongated.

Its inclination of 1.22° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 31.1 km/s at perihelion and falls to 24.7 km/s at aphelion.

Its perihelion lies just outside Earth's orbit, which is why it is classed as Earth-approaching rather than Earth-crossing.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 28.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 25 observations and has a weighted RMS residual of 0.4884 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
1.154 AU
Eccentricity
0.1136
Perihelion
1.023 AU
Aphelion
1.285094 AU
Inclination
1.22°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
139.29°

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
2030-Feb-27 05:14 0.269639 AU
40337490 km
4.89 km/s
2035-Apr-04 12:10 0.284059 AU
42494565 km
5.08 km/s
2040-May-12 07:54 0.242953 AU
36345213 km
4.18 km/s
2040-Nov-04 00:58 0.381258 AU
57035355 km
13.13 km/s
2045-Oct-21 21:00 0.104902 AU
15693096 km
5.10 km/s
2050-Aug-31 15:13 0.073163 AU
10945086 km
3.99 km/s
2055-Aug-11 09:49 0.381731 AU
57106105 km
12.77 km/s
2056-Feb-07 18:24 0.242084 AU
36215235 km
4.31 km/s
2061-Mar-21 08:42 0.283652 AU
42433715 km
5.11 km/s
2066-Nov-08 04:52 0.410504 AU
61410500 km
15.32 km/s
2071-Oct-25 12:57 0.082114 AU
12284096 km
6.46 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
28.9

Orbit Quality

RMS
0.48837
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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