SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 SE20

2017 SE20

2017 SE20 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.754 AU and a period of 0.66 yr.

Aten Observations: 23
Orbital Period · P
0.66 yr
v(q)
50.6 km/s
v(Q)
23.2 km/s
Diameter · ≈
0.01 km
TJ
7.6
Eccentricity · e
0.3706

Orbit and dynamics

The path is an ellipse reaching 0.475 AU from the Sun at perihelion and 1.034 AU at aphelion, a radial span of 0.559 AU.

Applying Kepler's third law to a = 0.754 AU gives an orbital period of 0.66 yr, or about 239 days.

An eccentricity of 0.371 makes the orbit moderately elongated.

The orbital plane is tilted 7.31° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 50.6 km/s at perihelion and falls to 23.2 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 = 27.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 23 observations and has a weighted RMS residual of 0.4814 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
0.7545 AU
Eccentricity
0.3706
Perihelion
0.475 AU
Aphelion
1.034118 AU
Inclination
7.31°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
251.63°

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-23 05:21 0.259214 AU
38777920 km
20.44 km/s
2034-Sep-18 01:12 0.059193 AU
8855113 km
14.16 km/s
2040-Nov-04 07:13 0.076876 AU
11500426 km
11.64 km/s
2042-Jun-10 21:32 0.445311 AU
66617575 km
13.71 km/s
2042-Nov-01 04:43 0.251540 AU
37629774 km
17.63 km/s
2044-Oct-24 22:35 0.455118 AU
68084690 km
23.67 km/s
2053-Sep-22 11:52 0.246657 AU
36899388 km
19.47 km/s
2055-Sep-18 00:46 0.042090 AU
6296581 km
13.51 km/s
2061-Nov-04 11:20 0.069191 AU
10350882 km
10.96 km/s
2063-Nov-02 17:00 0.102554 AU
15341927 km
16.39 km/s
2065-Oct-27 11:33 0.247209 AU
36981942 km
21.93 km/s
2074-Sep-27 22:28 0.290485 AU
43455975 km
24.08 km/s
2076-Sep-21 12:49 0.136066 AU
20355127 km
18.68 km/s
2078-Sep-17 20:48 0.022240 AU
3327099 km
13.39 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
27.9

Orbit Quality

RMS
0.48143
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.