SpaceAtlas Space Object Data
NASA JPL SBDB · 2000 LF3

2000 LF3

2000 LF3 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.598 AU it takes 4.19 yr to circle the Sun.

Apollo Observations: 198
Orbital Period · P
4.19 yr
v(q)
40.4 km/s
v(Q)
8.4 km/s
Diameter · ≈
0.17 km
TJ
3.04
Eccentricity · e
0.6544

Orbit and dynamics

Between its closest point (0.898 AU) and its farthest (4.298 AU), the heliocentric distance changes by 3.4 AU over every revolution.

One full revolution takes 4.19 yr (1,529 days), computed from the semi-major axis of 2.598 AU.

The high eccentricity (0.654) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.59° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.4 km/s at perihelion and falls to 8.4 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 = 21.61 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.17 km.

Observation record and orbit quality

Astrometry from 198 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4376 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
2.598 AU
Eccentricity
0.6544
Perihelion
0.898 AU
Aphelion
4.298131 AU
Inclination
14.59°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
76.7°

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
2046-Jun-14 08:18 0.007462 AU
1116347 km
15.15 km/s
2067-Jul-11 11:45 0.172051 AU
25738452 km
13.08 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
21.61

Orbit Quality

RMS
0.43756
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.

Keep exploring

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