SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 JN

2020 JN

2020 JN belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.181 AU it takes 1.28 yr to circle the Sun.

Apollo Observations: 41
Orbital Period · P
1.28 yr
v(q)
60.8 km/s
v(Q)
12.4 km/s
Diameter · ≈
0.01 km
TJ
5.12
Eccentricity · e
0.662

Orbit and dynamics

Between its closest point (0.399 AU) and its farthest (1.963 AU), the heliocentric distance changes by 1.564 AU over every revolution.

One full revolution takes 1.28 yr (469 days), computed from the semi-major axis of 1.181 AU.

The high eccentricity (0.662) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 2.79° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 60.8 km/s at perihelion and falls to 12.4 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 = 27.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

Astrometry from 41 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3835 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.181 AU
Eccentricity
0.662
Perihelion
0.399 AU
Aphelion
1.962822 AU
Inclination
2.79°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
229.8°

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-11 22:09 0.098708 AU
14766468 km
26.21 km/s
2029-Apr-30 17:28 0.043758 AU
6546156 km
25.36 km/s
2036-Jan-07 05:31 0.041845 AU
6259881 km
22.45 km/s
2038-Apr-26 18:51 0.134731 AU
20155464 km
28.42 km/s
2045-Jan-04 09:19 0.046623 AU
6974723 km
20.74 km/s
2047-Apr-24 06:35 0.274936 AU
41129901 km
30.40 km/s
2052-Jul-06 07:38 0.481860 AU
72085263 km
18.19 km/s
2054-Jan-01 19:29 0.081633 AU
12212096 km
18.25 km/s
2056-Apr-19 19:38 0.300177 AU
44905848 km
33.01 km/s
2061-May-06 10:22 0.341947 AU
51154494 km
12.88 km/s
2062-Dec-30 16:10 0.120862 AU
18080758 km
15.45 km/s
2065-Apr-15 19:25 0.342354 AU
51215454 km
36.04 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
27.4

Orbit Quality

RMS
0.38345
Condition
7
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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