SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 SV17

2017 SV17

2017 SV17 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.89 AU and a period of 0.84 yr.

Aten Observations: 23
Orbital Period · P
0.84 yr
v(q)
41.1 km/s
v(Q)
24.2 km/s
Diameter · ≈
0.03 km
TJ
6.64
Eccentricity · e
0.2588

Orbit and dynamics

Between its closest point (0.66 AU) and its farthest (1.121 AU), the heliocentric distance changes by 0.461 AU over every revolution.

One full revolution takes 0.84 yr (307 days), computed from the semi-major axis of 0.89 AU.

An eccentricity of 0.259 makes the orbit moderately elongated.

Its inclination of 4.98° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 41.1 km/s at perihelion and falls to 24.2 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 = 25.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

Astrometry from 23 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5013 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
0.8903 AU
Eccentricity
0.2588
Perihelion
0.66 AU
Aphelion
1.12071 AU
Inclination
4.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
253.63°

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
2027-Sep-27 02:15 0.364222 AU
54486836 km
20.12 km/s
2028-May-28 14:00 0.335430 AU
50179605 km
10.99 km/s
2028-Dec-25 01:48 0.085354 AU
12768833 km
9.25 km/s
2039-Mar-21 09:30 0.291254 AU
43570984 km
9.89 km/s
2043-Sep-17 13:30 0.072873 AU
10901690 km
11.45 km/s
2044-Apr-20 05:12 0.340453 AU
50930991 km
11.74 km/s
2044-Dec-15 02:10 0.315027 AU
47127400 km
18.55 km/s
2048-Sep-24 00:25 0.291760 AU
43646614 km
18.24 km/s
2049-May-20 00:42 0.342953 AU
51305062 km
11.48 km/s
2049-Dec-23 18:07 0.108903 AU
16291720 km
11.37 km/s
2064-Sep-15 20:07 0.026180 AU
3916416 km
9.22 km/s
2065-Dec-12 18:36 0.365730 AU
54712471 km
20.76 km/s
2069-Sep-22 16:54 0.284790 AU
42603938 km
16.90 km/s
2070-May-15 00:34 0.349044 AU
52216213 km
11.65 km/s
2070-Dec-23 03:51 0.189339 AU
28324685 km
12.59 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
25.7

Orbit Quality

RMS
0.50135
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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