SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 RH16

2017 RH16

2017 RH16 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.875 AU and a period of 0.82 yr.

Aten Observations: 41
Orbital Period · P
0.82 yr
v(q)
51.3 km/s
v(Q)
19.8 km/s
Diameter · ≈
0.02 km
TJ
6.69
Eccentricity · e
0.4429

Orbit and dynamics

The path is an ellipse reaching 0.487 AU from the Sun at perihelion and 1.262 AU at aphelion, a radial span of 0.775 AU.

Applying Kepler's third law to a = 0.875 AU gives an orbital period of 0.82 yr, or about 299 days.

The high eccentricity (0.443) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 0.62° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 51.3 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 = 26.14 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 41 observations and has a weighted RMS residual of 0.755 arcseconds.

Condition code U = 0 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
0.8747 AU
Eccentricity
0.4429
Perihelion
0.487 AU
Aphelion
1.262105 AU
Inclination
0.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
347.12°

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-Dec-04 17:37 0.115605 AU
17294206 km
16.32 km/s
2035-Sep-03 09:22 0.098211 AU
14692091 km
10.19 km/s
2036-Dec-01 06:03 0.196446 AU
29387866 km
18.92 km/s
2044-Sep-13 12:35 0.177795 AU
26597821 km
9.33 km/s
2049-Nov-25 08:33 0.167533 AU
25062593 km
9.38 km/s
2057-Sep-05 15:22 0.188088 AU
28137599 km
18.64 km/s
2058-Dec-04 18:09 0.096477 AU
14432749 km
10.17 km/s
2066-Sep-02 23:04 0.097212 AU
14542680 km
15.77 km/s
2067-Dec-07 08:03 0.013859 AU
2073213 km
12.47 km/s
2075-Sep-02 18:35 0.090383 AU
13521121 km
15.55 km/s
2076-Dec-06 16:08 0.019678 AU
2943796 km
12.24 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
26.14

Orbit Quality

RMS
0.75498
Condition
0
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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