SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 FM6

2020 FM6

2020 FM6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.364 AU it takes 1.59 yr to circle the Sun.

Apollo Observations: 204
Orbital Period · P
1.59 yr
v(q)
43.8 km/s
v(Q)
14.8 km/s
Diameter · ≈
0.15 km
TJ
4.68
Eccentricity · e
0.4939

Orbit and dynamics

The path is an ellipse reaching 0.69 AU from the Sun at perihelion and 2.038 AU at aphelion, a radial span of 1.348 AU.

Applying Kepler's third law to a = 1.364 AU gives an orbital period of 1.59 yr, or about 582 days.

The high eccentricity (0.494) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.98° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 43.8 km/s at perihelion and falls to 14.8 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 = 21.94 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.15 km.

Observation record and orbit quality

The current orbit solution is based on 204 observations and has a weighted RMS residual of 0.5272 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
1.364 AU
Eccentricity
0.4939
Perihelion
0.69 AU
Aphelion
2.03768 AU
Inclination
14.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
266.73°

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-Apr-17 08:13 0.222244 AU
33247181 km
22.80 km/s
2031-Sep-25 17:36 0.273357 AU
40893646 km
11.45 km/s
2036-Apr-06 18:37 0.453427 AU
67831681 km
29.51 km/s
2039-Aug-11 21:55 0.381651 AU
57094118 km
14.32 km/s
2047-Apr-30 23:25 0.456778 AU
68333034 km
8.59 km/s
2047-Jul-04 13:05 0.373136 AU
55820294 km
13.40 km/s
2050-Nov-13 11:18 0.385860 AU
57723763 km
27.75 km/s
2055-May-09 18:29 0.204953 AU
30660574 km
11.71 km/s
2058-Nov-02 02:04 0.144861 AU
21670927 km
20.80 km/s
2063-Apr-27 05:55 0.045270 AU
6772226 km
17.44 km/s
2066-Oct-20 17:06 0.086709 AU
12971520 km
14.65 km/s
2071-Apr-15 07:44 0.287999 AU
43083963 km
24.66 km/s
2074-Sep-07 16:55 0.326818 AU
48891210 km
12.65 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
21.94

Orbit Quality

RMS
0.52724
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.

Keep exploring

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