SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 LD2

2020 LD2

2020 LD2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.923 AU it takes 2.67 yr to circle the Sun.

Apollo Observations: 23
Orbital Period · P
2.67 yr
v(q)
36.8 km/s
v(Q)
12.5 km/s
Diameter · ≈
0.2 km
TJ
3.69
Eccentricity · e
0.4915

Orbit and dynamics

The path is an ellipse reaching 0.978 AU from the Sun at perihelion and 2.868 AU at aphelion, a radial span of 1.89 AU.

Applying Kepler's third law to a = 1.923 AU gives an orbital period of 2.67 yr, or about 974 days.

The high eccentricity (0.491) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 22.14° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36.8 km/s at perihelion and falls to 12.5 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 = 21.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

The current orbit solution is based on 23 observations and has a weighted RMS residual of 0.4231 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.923 AU
Eccentricity
0.4915
Perihelion
0.978 AU
Aphelion
2.868155 AU
Inclination
22.14°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
122.45°

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
2028-Jan-24 00:44 0.324307 AU
48515662 km
16.77 km/s
2028-May-28 09:13 0.411271 AU
61525283 km
10.84 km/s
2036-Jan-24 00:08 0.320922 AU
48009181 km
17.01 km/s
2036-May-28 17:24 0.389149 AU
58215902 km
10.85 km/s
2044-Jan-23 04:32 0.320491 AU
47944735 km
17.76 km/s
2044-May-30 04:32 0.365365 AU
54657814 km
10.85 km/s
2052-Jan-21 11:39 0.318746 AU
47683717 km
19.05 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
21.3

Orbit Quality

RMS
0.42306
Condition
6
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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