SpaceAtlas Space Object Data
NASA JPL SBDB · 221980

221980

221980 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.342 AU it takes 1.55 yr to circle the Sun.

Apollo Observations: 189
Orbital Period · P
1.55 yr
v(q)
39.3 km/s
v(Q)
16.8 km/s
Diameter · ≈
0.54 km
TJ
4.74
Eccentricity · e
0.4007

Orbit and dynamics

Between its closest point (0.804 AU) and its farthest (1.88 AU), the heliocentric distance changes by 1.076 AU over every revolution.

One full revolution takes 1.55 yr (568 days), computed from the semi-major axis of 1.342 AU.

The high eccentricity (0.401) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 21.59° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 39.3 km/s at perihelion and falls to 16.8 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

The measured diameter is 0.43 km, a value from direct size determination rather than from brightness alone.

A geometric albedo of 0.2 points to a comparatively bright, reflective surface.

Observation record and orbit quality

Astrometry from 189 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4695 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
1.342 AU
Eccentricity
0.4007
Perihelion
0.804 AU
Aphelion
1.879739 AU
Inclination
21.59°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
234.07°

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-Feb-24 09:27 0.291100 AU
43547930 km
19.21 km/s
2037-Sep-24 22:46 0.114987 AU
17201830 km
13.72 km/s
2041-Feb-22 02:27 0.248052 AU
37108031 km
17.45 km/s
2051-Sep-20 18:56 0.062752 AU
9387530 km
14.56 km/s
2055-Feb-21 18:18 0.229137 AU
34278386 km
16.46 km/s
2065-Sep-20 22:51 0.070237 AU
10507364 km
14.43 km/s
2069-Feb-21 14:04 0.236449 AU
35372220 km
16.89 km/s
2079-Sep-25 09:33 0.114184 AU
17081643 km
13.71 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
0.432 km
Albedo
0.2
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
19.11

Orbit Quality

RMS
0.46947
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.

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