SpaceAtlas Space Object Data
NASA JPL SBDB · 2022 ES4

2022 ES4

2022 ES4 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.224 AU it takes 1.35 yr to circle the Sun.

Apollo Observations: 39
Orbital Period · P
1.35 yr
v(q)
38.6 km/s
v(Q)
18.8 km/s
Diameter · ≈
0.02 km
TJ
5.16
Eccentricity · e
0.3458

Orbit and dynamics

The path is an ellipse reaching 0.8 AU from the Sun at perihelion and 1.647 AU at aphelion, a radial span of 0.847 AU.

Applying Kepler's third law to a = 1.224 AU gives an orbital period of 1.35 yr, or about 495 days.

An eccentricity of 0.346 makes the orbit moderately elongated.

Its inclination of 2.93° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.6 km/s at perihelion and falls to 18.8 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 = 26.47 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 39 observations and has a weighted RMS residual of 0.3514 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.224 AU
Eccentricity
0.3458
Perihelion
0.8 AU
Aphelion
1.647259 AU
Inclination
2.93°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
93.88°

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
2032-Sep-12 13:44 0.289585 AU
43321232 km
21.49 km/s
2040-Sep-12 07:53 0.281848 AU
42163801 km
5.11 km/s
2040-Dec-13 10:11 0.182684 AU
27329135 km
8.30 km/s
2041-Apr-09 15:17 0.340497 AU
50937611 km
6.28 km/s
2044-Aug-06 23:39 0.462529 AU
69193374 km
8.59 km/s
2045-Mar-03 21:01 0.006388 AU
955629 km
8.49 km/s
2049-Mar-22 04:40 0.194968 AU
29166848 km
17.30 km/s
2059-Sep-17 10:16 0.321203 AU
48051240 km
18.97 km/s
2063-Oct-03 14:57 0.021920 AU
3279172 km
10.29 km/s
2067-Nov-22 00:53 0.160231 AU
23970281 km
7.54 km/s
2068-Apr-20 23:58 0.407606 AU
60977001 km
7.37 km/s
2071-Aug-23 09:47 0.394584 AU
59028884 km
7.24 km/s
2072-Jan-17 11:37 0.164062 AU
24543356 km
7.70 km/s
2076-Mar-08 13:56 0.007076 AU
1058603 km
10.06 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
26.47

Orbit Quality

RMS
0.35137
Condition
7
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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