SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 MR3

2020 MR3

2020 MR3 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.818 AU and a period of 0.74 yr.

Aten Observations: 44
Orbital Period · P
0.74 yr
v(q)
66.5 km/s
v(Q)
16.3 km/s
Diameter · ≈
0.1 km
TJ
6.98
Eccentricity · e
0.606

Orbit and dynamics

The path is an ellipse reaching 0.322 AU from the Sun at perihelion and 1.314 AU at aphelion, a radial span of 0.992 AU.

Applying Kepler's third law to a = 0.818 AU gives an orbital period of 0.74 yr, or about 270 days.

The high eccentricity (0.606) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.3° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 66.5 km/s at perihelion and falls to 16.3 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 = 22.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.1 km.

Observation record and orbit quality

The current orbit solution is based on 44 observations and has a weighted RMS residual of 0.5897 arcseconds.

Condition code U = 1 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
0.8184 AU
Eccentricity
0.606
Perihelion
0.322 AU
Aphelion
1.31435 AU
Inclination
8.3°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
225.53°

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
2028-May-18 03:29 0.116785 AU
17470786 km
14.98 km/s
2040-Jul-25 21:50 0.159716 AU
23893213 km
13.65 km/s
2043-Jul-30 00:15 0.092914 AU
13899798 km
18.46 km/s
2045-May-18 19:01 0.114878 AU
17185535 km
18.67 km/s
2048-May-21 15:05 0.165765 AU
24798094 km
13.67 km/s
2060-Jul-29 15:55 0.098670 AU
14760868 km
15.17 km/s
2063-Jul-27 18:46 0.164703 AU
24639258 km
21.30 km/s
2065-May-18 00:31 0.098274 AU
14701605 km
16.08 km/s
2077-Jul-23 05:58 0.189708 AU
28379847 km
13.31 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
22.7

Orbit Quality

RMS
0.58971
Condition
1
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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