SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 YS2

2020 YS2

2020 YS2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.106 AU it takes 1.16 yr to circle the Sun.

Apollo Observations: 24
Orbital Period · P
1.16 yr
v(q)
32.2 km/s
v(Q)
24.9 km/s
TJ
5.62
Eccentricity · e
0.1279

Orbit and dynamics

Between its closest point (0.964 AU) and its farthest (1.247 AU), the heliocentric distance changes by 0.283 AU over every revolution.

One full revolution takes 1.16 yr (425 days), computed from the semi-major axis of 1.106 AU.

An eccentricity of 0.128 makes the orbit moderately elongated.

Its inclination of 0.73° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.2 km/s at perihelion and falls to 24.9 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

Neither a measured diameter nor a reliable absolute magnitude is available for 2020 YS2, so its physical size remains unconstrained.

Observation record and orbit quality

Astrometry from 24 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4655 arcseconds.

Condition code U = 5 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
1.106 AU
Eccentricity
0.1279
Perihelion
0.964 AU
Aphelion
1.247457 AU
Inclination
0.73°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
280.96°

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-Sep-16 14:50 0.048020 AU
7183636 km
4.15 km/s
2028-Feb-24 13:14 0.149280 AU
22332011 km
2.66 km/s
2034-Aug-26 03:11 0.366319 AU
54800519 km
13.68 km/s
2035-Apr-30 00:58 0.230331 AU
34456966 km
4.50 km/s
2042-Jun-25 12:27 0.191464 AU
28642622 km
3.67 km/s
2043-Jan-09 10:29 0.153035 AU
22893700 km
7.86 km/s
2049-Sep-22 02:03 0.012263 AU
1834548 km
3.11 km/s
2050-Feb-18 23:18 0.120785 AU
18069166 km
2.22 km/s
2064-Aug-24 13:22 0.327456 AU
48986782 km
14.88 km/s
2066-Jan-24 18:02 0.263354 AU
39397227 km
15.12 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
31.07

Orbit Quality

RMS
0.46553
Condition
5
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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