SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 RE3

2019 RE3

2019 RE3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.024 AU it takes 1.04 yr to circle the Sun.

Apollo Observations: 28
Orbital Period · P
1.04 yr
v(q)
43.7 km/s
v(Q)
19.8 km/s
Diameter · ≈
0.1 km
TJ
5.84
Eccentricity · e
0.3757

Orbit and dynamics

The path is an ellipse reaching 0.639 AU from the Sun at perihelion and 1.409 AU at aphelion, a radial span of 0.77 AU.

Applying Kepler's third law to a = 1.024 AU gives an orbital period of 1.04 yr, or about 378 days.

An eccentricity of 0.376 makes the orbit moderately elongated.

A steep inclination of 23.33° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 43.7 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

No direct size measurement is available; from an absolute magnitude of H = 22.85 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 28 observations and has a weighted RMS residual of 0.5168 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

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
1.024 AU
Eccentricity
0.3757
Perihelion
0.639 AU
Aphelion
1.408717 AU
Inclination
23.33°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
80.63°

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-May-16 23:24 0.385534 AU
57675099 km
20.73 km/s
2046-Sep-27 00:45 0.433218 AU
64808521 km
25.33 km/s
2047-Oct-03 19:10 0.247496 AU
37024910 km
19.68 km/s
2048-Oct-05 10:09 0.140344 AU
20995169 km
15.16 km/s
2049-Sep-29 10:29 0.229577 AU
34344275 km
13.13 km/s
2050-Sep-16 22:53 0.355032 AU
53112051 km
13.00 km/s
2051-Jan-15 17:06 0.443672 AU
66372316 km
15.63 km/s
2051-Sep-02 12:55 0.452918 AU
67755598 km
13.03 km/s
2052-Feb-13 09:34 0.395469 AU
59161300 km
18.11 km/s
2053-Mar-09 19:44 0.328044 AU
49074635 km
18.04 km/s
2054-Apr-03 11:12 0.276567 AU
41373857 km
17.38 km/s
2055-Apr-27 03:28 0.289718 AU
43341250 km
17.87 km/s
2056-May-16 13:56 0.387572 AU
57979995 km
20.79 km/s
2075-Sep-26 22:42 0.444261 AU
66460555 km
25.65 km/s
2076-Oct-02 21:05 0.257734 AU
38556467 km
19.99 km/s
2077-Oct-05 20:07 0.141440 AU
21159066 km
15.38 km/s
2078-Sep-30 13:05 0.219966 AU
32906442 km
13.19 km/s
2079-Sep-18 10:24 0.345590 AU
51699534 km
12.98 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
22.85

Orbit Quality

RMS
0.51678
Condition
1
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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