SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 PE2

2019 PE2

2019 PE2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.332 AU it takes 1.54 yr to circle the Sun.

Apollo Observations: 229
Orbital Period · P
1.54 yr
v(q)
38.4 km/s
v(Q)
17.3 km/s
Diameter · ≈
0.28 km
TJ
4.69
Eccentricity · e
0.3779

Orbit and dynamics

The path is an ellipse reaching 0.829 AU from the Sun at perihelion and 1.835 AU at aphelion, a radial span of 1.006 AU.

Applying Kepler's third law to a = 1.332 AU gives an orbital period of 1.54 yr, or about 561 days.

An eccentricity of 0.378 makes the orbit moderately elongated.

A steep inclination of 32.84° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 38.4 km/s at perihelion and falls to 17.3 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 = 20.48 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.28 km.

Observation record and orbit quality

The current orbit solution is based on 229 observations and has a weighted RMS residual of 0.4084 arcseconds.

Condition code U = 0 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
1.332 AU
Eccentricity
0.3779
Perihelion
0.829 AU
Aphelion
1.835363 AU
Inclination
32.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
93.36°

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
2039-Sep-09 15:23 0.168678 AU
25233851 km
20.07 km/s
2042-Sep-09 15:41 0.404285 AU
60480206 km
16.12 km/s
2043-Feb-21 02:04 0.195264 AU
29211095 km
17.52 km/s
2046-Mar-07 01:55 0.302578 AU
45264965 km
25.18 km/s
2059-Sep-09 11:36 0.172044 AU
25737353 km
20.20 km/s
2062-Sep-09 19:01 0.399312 AU
59736204 km
16.13 km/s
2063-Feb-21 01:17 0.200240 AU
29955528 km
17.48 km/s
2066-Mar-07 00:16 0.298724 AU
44688450 km
25.11 km/s
2079-Sep-09 16:43 0.169724 AU
25390277 km
20.07 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
20.48

Orbit Quality

RMS
0.40843
Condition
0
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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