SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 SG17

2016 SG17

2016 SG17 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.019 AU it takes 1.03 yr to circle the Sun.

Apollo Observations: 80
Orbital Period · P
1.03 yr
v(q)
36 km/s
v(Q)
24.2 km/s
Diameter · ≈
0.16 km
TJ
5.85
Eccentricity · e
0.1959

Orbit and dynamics

Between its closest point (0.819 AU) and its farthest (1.219 AU), the heliocentric distance changes by 0.4 AU over every revolution.

One full revolution takes 1.03 yr (376 days), computed from the semi-major axis of 1.019 AU.

An eccentricity of 0.196 makes the orbit moderately elongated.

A steep inclination of 31.73° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 36 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 = 21.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.16 km.

Observation record and orbit quality

Astrometry from 80 individual observations underpins this orbit; the fit leaves an RMS residual of 0.6903 arcseconds.

Condition code U = 1 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
1.019 AU
Eccentricity
0.1959
Perihelion
0.819 AU
Aphelion
1.218622 AU
Inclination
31.73°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
308.21°

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
2049-Feb-23 08:07 0.468070 AU
70022350 km
23.18 km/s
2049-Oct-31 06:58 0.494912 AU
74037825 km
17.30 km/s
2050-Mar-09 14:37 0.331369 AU
49572122 km
20.97 km/s
2050-Oct-24 00:02 0.398428 AU
59604036 km
16.54 km/s
2051-Mar-23 21:46 0.217820 AU
32585334 km
19.50 km/s
2051-Oct-17 20:51 0.309453 AU
46293505 km
15.99 km/s
2052-Apr-06 09:39 0.179418 AU
26840492 km
18.90 km/s
2052-Oct-11 11:12 0.238773 AU
35719918 km
15.73 km/s
2053-Apr-21 09:09 0.249200 AU
37279848 km
19.09 km/s
2053-Oct-06 15:00 0.210031 AU
31420122 km
15.83 km/s
2054-May-07 09:27 0.366016 AU
54755197 km
19.83 km/s
2054-Oct-02 08:24 0.243668 AU
36452172 km
16.40 km/s
2055-May-25 17:18 0.492160 AU
73626024 km
20.58 km/s
2055-Sep-28 21:57 0.325674 AU
48720138 km
17.58 km/s
2056-Sep-25 16:37 0.433202 AU
64806047 km
19.50 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
21.7

Orbit Quality

RMS
0.69034
Condition
1
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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