SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 TU5

2020 TU5

2020 TU5 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.59 AU it takes 2.00 yr to circle the Sun.

Apollo Observations: 50
Orbital Period · P
2.00 yr
v(q)
34.5 km/s
v(Q)
16.2 km/s
Diameter · ≈
0.3 km
TJ
3.84
Eccentricity · e
0.3628

Orbit and dynamics

Between its closest point (1.013 AU) and its farthest (2.167 AU), the heliocentric distance changes by 1.154 AU over every revolution.

One full revolution takes 2.00 yr (732 days), computed from the semi-major axis of 1.59 AU.

An eccentricity of 0.363 makes the orbit moderately elongated.

A steep inclination of 56.83° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 34.5 km/s at perihelion and falls to 16.2 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 20.36 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.3 km.

Observation record and orbit quality

Astrometry from 50 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5451 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
1.59 AU
Eccentricity
0.3628
Perihelion
1.013 AU
Aphelion
2.166852 AU
Inclination
56.83°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
303.12°

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
2040-Oct-28 04:51 0.199909 AU
29905967 km
30.85 km/s
2042-Oct-29 07:43 0.183967 AU
27521135 km
30.82 km/s
2044-Oct-29 05:38 0.173583 AU
25967617 km
30.80 km/s
2046-Oct-30 03:05 0.163548 AU
24466490 km
30.80 km/s
2048-Oct-29 23:53 0.154449 AU
23105167 km
30.79 km/s
2050-Oct-30 17:06 0.148899 AU
22274969 km
30.77 km/s
2052-Oct-30 08:29 0.145249 AU
21728956 km
30.78 km/s
2054-Oct-31 00:59 0.141004 AU
21093943 km
30.78 km/s
2056-Oct-30 11:58 0.142359 AU
21296623 km
30.77 km/s
2058-Oct-30 22:27 0.143807 AU
21513187 km
30.78 km/s
2060-Oct-30 08:07 0.146762 AU
21955272 km
30.78 km/s
2062-Oct-30 14:01 0.153782 AU
23005459 km
30.78 km/s
2064-Oct-29 18:10 0.162247 AU
24271798 km
30.79 km/s
2066-Oct-29 23:16 0.169999 AU
25431458 km
30.79 km/s
2068-Oct-28 23:31 0.183058 AU
27385157 km
30.82 km/s
2070-Oct-28 23:46 0.195923 AU
29309679 km
30.85 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
20.36

Orbit Quality

RMS
0.54505
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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