SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 SD20

2017 SD20

2017 SD20 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.852 AU and a period of 0.79 yr.

Aten Observations: 39
Orbital Period · P
0.79 yr
v(q)
52.6 km/s
v(Q)
19.8 km/s
Diameter · ≈
0.02 km
TJ
6.83
Eccentricity · e
0.453

Orbit and dynamics

Between its closest point (0.466 AU) and its farthest (1.238 AU), the heliocentric distance changes by 0.772 AU over every revolution.

One full revolution takes 0.79 yr (287 days), computed from the semi-major axis of 0.852 AU.

The high eccentricity (0.453) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.48° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 52.6 km/s at perihelion and falls to 19.8 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 = 25.97 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 39 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6524 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
0.8518 AU
Eccentricity
0.453
Perihelion
0.466 AU
Aphelion
1.237665 AU
Inclination
6.48°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
116.41°

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-Sep-24 03:17 0.029703 AU
4443441 km
14.46 km/s
2036-Dec-10 08:20 0.186879 AU
27956719 km
9.81 km/s
2039-Sep-26 21:39 0.116452 AU
17421016 km
17.16 km/s
2051-Dec-22 13:24 0.140042 AU
20949926 km
16.10 km/s
2054-Oct-01 02:25 0.134826 AU
20169729 km
10.23 km/s
2062-Dec-24 01:33 0.111004 AU
16605929 km
13.29 km/s
2065-Sep-25 05:52 0.066069 AU
9883736 km
11.52 km/s
2073-Dec-23 05:28 0.121939 AU
18241787 km
11.46 km/s
2076-Sep-24 00:39 0.012895 AU
1929000 km
13.01 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
25.97

Orbit Quality

RMS
0.65242
Condition
6
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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