SpaceAtlas Space Object Data
NASA JPL SBDB · 2018 LV2

2018 LV2

2018 LV2 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.992 AU and a period of 0.99 yr.

Aten Observations: 44
Orbital Period · P
0.99 yr
v(q)
40.7 km/s
v(Q)
22 km/s
Diameter · ≈
0.03 km
TJ
6.08
Eccentricity · e
0.2992

Orbit and dynamics

The path is an ellipse reaching 0.695 AU from the Sun at perihelion and 1.289 AU at aphelion, a radial span of 0.594 AU.

Applying Kepler's third law to a = 0.992 AU gives an orbital period of 0.99 yr, or about 361 days.

An eccentricity of 0.299 makes the orbit moderately elongated.

Its inclination of 2.98° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 40.7 km/s at perihelion and falls to 22 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 = 25.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 44 observations and has a weighted RMS residual of 0.5108 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
0.9919 AU
Eccentricity
0.2992
Perihelion
0.695 AU
Aphelion
1.288676 AU
Inclination
2.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
119.94°

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-Jan-30 04:21 0.288666 AU
43183884 km
10.41 km/s
2027-Aug-28 03:43 0.264307 AU
39539761 km
7.34 km/s
2028-Jan-18 19:18 0.278090 AU
41601722 km
9.92 km/s
2028-Sep-06 11:58 0.244093 AU
36515825 km
7.05 km/s
2029-Jan-05 16:13 0.260116 AU
38912741 km
9.07 km/s
2029-Sep-17 19:11 0.213311 AU
31910928 km
6.62 km/s
2029-Dec-22 21:27 0.232299 AU
34751368 km
7.78 km/s
2030-Oct-01 21:33 0.164749 AU
24646088 km
5.99 km/s
2031-Oct-19 01:21 0.095765 AU
14326182 km
5.65 km/s
2032-Oct-24 00:09 0.021324 AU
3189995 km
7.29 km/s
2033-Oct-23 00:14 0.011851 AU
1772922 km
9.31 km/s
2034-Oct-20 08:07 0.091590 AU
13701710 km
11.82 km/s
2035-Oct-17 00:24 0.192752 AU
28835264 km
14.46 km/s
2036-Oct-12 12:25 0.266786 AU
39910662 km
17.13 km/s
2037-Oct-08 22:15 0.340350 AU
50915688 km
19.79 km/s
2038-Oct-05 05:36 0.413623 AU
61877119 km
22.43 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
25.3

Orbit Quality

RMS
0.51077
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.

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