SpaceAtlas Space Object Data
NASA JPL SBDB · 2004 PE20

2004 PE20

2004 PE20 is an Amor-type near-Earth asteroid that approaches Earth from beyond our orbit without crossing it, orbiting the Sun at 2.212 AU once every 3.29 yr.

Amor Observations: 235
Orbital Period · P
3.29 yr
v(q)
31.8 km/s
v(Q)
12.6 km/s
Diameter · ≈
0.34 km
TJ
3.53
Eccentricity · e
0.4306

Orbit and dynamics

The path is an ellipse reaching 1.259 AU from the Sun at perihelion and 3.164 AU at aphelion, a radial span of 1.905 AU.

Applying Kepler's third law to a = 2.212 AU gives an orbital period of 3.29 yr, or about 1,202 days.

The high eccentricity (0.431) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.24° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 31.8 km/s at perihelion and falls to 12.6 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 = 20.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.34 km.

Observation record and orbit quality

The current orbit solution is based on 235 observations and has a weighted RMS residual of 0.4117 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
2.212 AU
Eccentricity
0.4306
Perihelion
1.259 AU
Aphelion
3.164487 AU
Inclination
4.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
218.3°

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-Aug-18 11:52 0.379667 AU
56797352 km
2.96 km/s
2037-Oct-09 17:36 0.499386 AU
74707115 km
1.92 km/s
2060-Sep-12 18:31 0.297513 AU
44507303 km
3.17 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
20.1

Orbit Quality

RMS
0.41174
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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