SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 EF

2019 EF

2019 EF belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.514 AU it takes 1.86 yr to circle the Sun.

Apollo Observations: 62
Orbital Period · P
1.86 yr
v(q)
47.6 km/s
v(Q)
12.3 km/s
Diameter · ≈
0.02 km
TJ
4.3
Eccentricity · e
0.5892

Orbit and dynamics

The path is an ellipse reaching 0.622 AU from the Sun at perihelion and 2.406 AU at aphelion, a radial span of 1.784 AU.

Applying Kepler's third law to a = 1.514 AU gives an orbital period of 1.86 yr, or about 680 days.

The high eccentricity (0.589) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 7.85° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 47.6 km/s at perihelion and falls to 12.3 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 = 26.71 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 62 observations and has a weighted RMS residual of 0.6182 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.514 AU
Eccentricity
0.5892
Perihelion
0.622 AU
Aphelion
2.406049 AU
Inclination
7.85°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
353.56°

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-17 01:43 0.108922 AU
16294554 km
13.03 km/s
2061-Oct-12 17:54 0.290161 AU
43407509 km
13.04 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
26.71

Orbit Quality

RMS
0.61825
Condition
7
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.

Keep exploring

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