SpaceAtlas Space Object Data
NASA JPL SBDB · 2012 TN20

2012 TN20

2012 TN20 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.183 AU it takes 1.29 yr to circle the Sun.

Apollo Observations: 44
Orbital Period · P
1.29 yr
v(q)
41.2 km/s
v(Q)
18.2 km/s
Diameter · ≈
0.12 km
TJ
5.26
Eccentricity · e
0.3859

Orbit and dynamics

Between its closest point (0.726 AU) and its farthest (1.64 AU), the heliocentric distance changes by 0.914 AU over every revolution.

One full revolution takes 1.29 yr (470 days), computed from the semi-major axis of 1.183 AU.

An eccentricity of 0.386 makes the orbit moderately elongated.

The orbital plane is tilted 11.62° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 41.2 km/s at perihelion and falls to 18.2 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 = 22.39 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

Astrometry from 44 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4265 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
1.183 AU
Eccentricity
0.3859
Perihelion
0.726 AU
Aphelion
1.63952 AU
Inclination
11.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
160.31°

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-Apr-15 13:20 0.137932 AU
20634366 km
11.90 km/s
2030-Oct-27 21:39 0.161565 AU
24169760 km
10.25 km/s
2036-Apr-17 00:10 0.138168 AU
20669659 km
12.27 km/s
2039-Oct-28 09:12 0.166373 AU
24888987 km
9.95 km/s
2045-Apr-16 16:27 0.138528 AU
20723547 km
12.13 km/s
2048-Oct-27 15:38 0.163193 AU
24413367 km
10.16 km/s
2054-Apr-15 04:47 0.138791 AU
20762799 km
11.84 km/s
2057-Oct-27 10:31 0.154518 AU
23115608 km
10.94 km/s
2063-Apr-10 02:27 0.145852 AU
21819131 km
11.18 km/s
2066-Oct-26 11:53 0.152173 AU
22764827 km
12.20 km/s
2072-Apr-01 07:49 0.163520 AU
24462242 km
10.77 km/s
2075-Oct-24 23:45 0.167535 AU
25062845 km
13.81 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
22.39

Orbit Quality

RMS
0.42647
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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