SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 PT4

2020 PT4

2020 PT4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.594 AU it takes 2.01 yr to circle the Sun.

Apollo Observations: 47
Orbital Period · P
2.01 yr
v(q)
40.3 km/s
v(Q)
13.8 km/s
Diameter · ≈
0.04 km
TJ
4.23
Eccentricity · e
0.49

Orbit and dynamics

The path is an ellipse reaching 0.813 AU from the Sun at perihelion and 2.375 AU at aphelion, a radial span of 1.562 AU.

Applying Kepler's third law to a = 1.594 AU gives an orbital period of 2.01 yr, or about 735 days.

The high eccentricity (0.49) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 3.97° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 40.3 km/s at perihelion and falls to 13.8 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 = 24.82 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

The current orbit solution is based on 47 observations and has a weighted RMS residual of 0.5101 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
1.594 AU
Eccentricity
0.49
Perihelion
0.813 AU
Aphelion
2.37506 AU
Inclination
3.97°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
285.56°

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
2027-Jan-29 06:53 0.485430 AU
72619245 km
4.09 km/s
2028-Nov-05 16:15 0.183340 AU
27427244 km
10.22 km/s
2030-Nov-25 06:37 0.182430 AU
27291104 km
10.12 km/s
2032-Dec-14 14:49 0.155512 AU
23264196 km
9.41 km/s
2035-Jan-03 17:06 0.104000 AU
15558162 km
9.57 km/s
2037-Jan-14 12:28 0.052433 AU
7843822 km
11.68 km/s
2039-Jan-21 12:58 0.082517 AU
12344349 km
14.09 km/s
2041-Jan-26 16:52 0.162391 AU
24293382 km
16.80 km/s
2043-Feb-01 17:33 0.257518 AU
38524089 km
19.76 km/s
2045-Feb-06 03:04 0.353658 AU
52906533 km
22.66 km/s
2047-Feb-11 11:28 0.448912 AU
67156206 km
25.56 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
24.82

Orbit Quality

RMS
0.51006
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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