SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 RT8

2020 RT8

2020 RT8 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.946 AU and a period of 0.92 yr.

Aten Observations: 17
Orbital Period · P
0.92 yr
v(q)
42.9 km/s
v(Q)
21.8 km/s
Diameter · ≈
0.05 km
TJ
6.31
Eccentricity · e
0.3259

Orbit and dynamics

Between its closest point (0.638 AU) and its farthest (1.254 AU), the heliocentric distance changes by 0.616 AU over every revolution.

One full revolution takes 0.92 yr (336 days), computed from the semi-major axis of 0.946 AU.

An eccentricity of 0.326 makes the orbit moderately elongated.

Its inclination of 3.23° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 42.9 km/s at perihelion and falls to 21.8 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

No direct size measurement is available; from an absolute magnitude of H = 24.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 17 individual observations underpins this orbit; the fit leaves an RMS residual of 0.8761 arcseconds.

Condition code U = 6 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
0.9459 AU
Eccentricity
0.3259
Perihelion
0.638 AU
Aphelion
1.254169 AU
Inclination
3.23°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
215.81°

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
2031-Aug-14 13:58 0.050812 AU
7601402 km
10.40 km/s
2032-May-20 09:04 0.324666 AU
48569416 km
11.34 km/s
2032-Oct-10 12:36 0.252078 AU
37710396 km
8.13 km/s
2033-Mar-18 13:05 0.342363 AU
51216740 km
12.45 km/s
2033-Dec-15 19:09 0.048495 AU
7254729 km
8.63 km/s
2034-Nov-29 16:34 0.407317 AU
60933711 km
23.72 km/s
2042-Aug-27 01:15 0.373847 AU
55926732 km
21.90 km/s
2043-Aug-13 04:49 0.051785 AU
7746874 km
8.29 km/s
2044-May-12 00:12 0.338789 AU
50682136 km
12.04 km/s
2044-Oct-15 03:35 0.255897 AU
38281702 km
8.21 km/s
2045-Mar-13 20:06 0.324309 AU
48515878 km
12.11 km/s
2045-Dec-15 16:48 0.047629 AU
7125213 km
8.86 km/s
2046-Nov-30 04:32 0.336578 AU
50351318 km
23.17 km/s
2055-Aug-14 18:34 0.049127 AU
7349271 km
12.44 km/s
2058-Dec-06 00:02 0.125920 AU
18837299 km
18.62 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
24.4

Orbit Quality

RMS
0.87611
Condition
6
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.

Keep exploring

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