SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 PY4

2020 PY4

2020 PY4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 2.53 AU it takes 4.02 yr to circle the Sun.

Apollo Observations: 35
Orbital Period · P
4.02 yr
v(q)
57.3 km/s
v(Q)
6.1 km/s
Diameter · ≈
0.2 km
TJ
2.87
Eccentricity · e
0.807

Orbit and dynamics

Between its closest point (0.488 AU) and its farthest (4.572 AU), the heliocentric distance changes by 4.084 AU over every revolution.

One full revolution takes 4.02 yr (1,470 days), computed from the semi-major axis of 2.53 AU.

The high eccentricity (0.807) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 8.61° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 57.3 km/s at perihelion and falls to 6.1 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 = 21.24 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.2 km.

Observation record and orbit quality

Astrometry from 35 individual observations underpins this orbit; the fit leaves an RMS residual of 0.7012 arcseconds.

Condition code U = 2 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
2.53 AU
Eccentricity
0.807
Perihelion
0.488 AU
Aphelion
4.57171 AU
Inclination
8.61°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
179.75°

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-Jul-29 14:13 0.045949 AU
6873813 km
25.16 km/s
2032-Aug-06 08:55 0.134681 AU
20148020 km
29.60 km/s
2036-Aug-11 04:24 0.198880 AU
29752072 km
31.93 km/s
2040-Aug-08 19:59 0.147668 AU
22090824 km
30.46 km/s
2044-Aug-07 14:25 0.125322 AU
18747936 km
29.74 km/s
2048-Aug-03 16:15 0.022773 AU
3406818 km
26.86 km/s
2052-Jul-20 13:28 0.236034 AU
35310181 km
19.83 km/s
2056-Jun-18 00:00 0.433174 AU
64801969 km
18.73 km/s
2068-Feb-06 23:45 0.361192 AU
54033612 km
17.77 km/s
2071-Dec-31 06:21 0.153647 AU
22985199 km
31.52 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
21.24

Orbit Quality

RMS
0.70117
Condition
2
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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