SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 NK1

2020 NK1

2020 NK1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.393 AU it takes 1.64 yr to circle the Sun.

Apollo Observations: 135
Orbital Period · P
1.64 yr
v(q)
54.5 km/s
v(Q)
11.7 km/s
Diameter · ≈
0.58 km
TJ
4.29
Eccentricity · e
0.6471

Orbit and dynamics

Between its closest point (0.492 AU) and its farthest (2.294 AU), the heliocentric distance changes by 1.802 AU over every revolution.

One full revolution takes 1.64 yr (601 days), computed from the semi-major axis of 1.393 AU.

The high eccentricity (0.647) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 45.45° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 54.5 km/s at perihelion and falls to 11.7 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 = 18.95 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.58 km.

Observation record and orbit quality

Astrometry from 135 individual observations underpins this orbit; the fit leaves an RMS residual of 0.354 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
1.393 AU
Eccentricity
0.6471
Perihelion
0.492 AU
Aphelion
2.29441 AU
Inclination
45.45°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
171.08°

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
2029-Jan-06 01:20 0.491617 AU
73544868 km
28.75 km/s
2038-Aug-17 12:55 0.425154 AU
63602157 km
22.57 km/s
2042-Mar-07 05:55 0.478329 AU
71556980 km
41.18 km/s
2043-Aug-04 20:02 0.023208 AU
3471809 km
29.13 km/s
2047-Feb-12 20:09 0.261963 AU
39189099 km
33.29 km/s
2048-Jul-19 06:45 0.336608 AU
50355912 km
37.69 km/s
2052-Jan-17 19:42 0.401912 AU
60125165 km
29.04 km/s
2066-Aug-12 16:46 0.243427 AU
36416115 km
25.02 km/s
2070-Feb-26 07:20 0.364747 AU
54565341 km
37.71 km/s
2071-Jul-29 20:06 0.120676 AU
18052799 km
32.31 km/s
2075-Feb-03 10:46 0.275433 AU
41204248 km
31.14 km/s
2076-Jul-12 18:00 0.473220 AU
70792766 km
41.39 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
18.95

Orbit Quality

RMS
0.35401
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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