SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 RB16

2017 RB16

2017 RB16 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.041 AU it takes 1.06 yr to circle the Sun.

Apollo Observations: 19
Orbital Period · P
1.06 yr
v(q)
40.2 km/s
v(Q)
21.2 km/s
Diameter · ≈
0.03 km
TJ
5.85
Eccentricity · e
0.31

Orbit and dynamics

The path is an ellipse reaching 0.718 AU from the Sun at perihelion and 1.364 AU at aphelion, a radial span of 0.646 AU.

Applying Kepler's third law to a = 1.041 AU gives an orbital period of 1.06 yr, or about 388 days.

An eccentricity of 0.31 makes the orbit moderately elongated.

The orbital plane is tilted 5.17° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 40.2 km/s at perihelion and falls to 21.2 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 = 25.6 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 19 observations and has a weighted RMS residual of 0.3372 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
1.041 AU
Eccentricity
0.31
Perihelion
0.718 AU
Aphelion
1.36371 AU
Inclination
5.17°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
3.65°

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
2033-Sep-06 10:58 0.366970 AU
54897999 km
22.26 km/s
2034-Sep-24 03:17 0.009702 AU
1451371 km
11.10 km/s
2036-Jul-08 22:55 0.359166 AU
53730463 km
8.08 km/s
2037-May-27 02:01 0.267320 AU
39990437 km
6.91 km/s
2038-Apr-16 08:23 0.024712 AU
3696905 km
9.90 km/s
2039-May-04 12:56 0.359489 AU
53778724 km
21.03 km/s
2051-Sep-19 20:52 0.106508 AU
15933412 km
14.19 km/s
2053-Jul-19 04:52 0.345148 AU
51633460 km
8.01 km/s
2055-Apr-12 18:09 0.024080 AU
3602291 km
7.78 km/s
2056-Apr-30 08:28 0.245225 AU
36685135 km
18.83 km/s
2068-Sep-16 07:55 0.162100 AU
24249772 km
16.15 km/s
2070-Jul-24 21:01 0.334521 AU
50043592 km
7.91 km/s
2072-Apr-09 14:42 0.021749 AU
3253638 km
6.71 km/s
2073-Apr-29 03:45 0.206666 AU
30916749 km
17.95 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
25.6

Orbit Quality

RMS
0.3372
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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