SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 NR6

2017 NR6

2017 NR6 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.32 AU it takes 1.52 yr to circle the Sun.

Apollo Observations: 49
Orbital Period · P
1.52 yr
v(q)
44.4 km/s
v(Q)
15.1 km/s
Diameter · ≈
0.13 km
TJ
4.82
Eccentricity · e
0.492

Orbit and dynamics

The path is an ellipse reaching 0.671 AU from the Sun at perihelion and 1.969 AU at aphelion, a radial span of 1.298 AU.

Applying Kepler's third law to a = 1.32 AU gives an orbital period of 1.52 yr, or about 554 days.

The high eccentricity (0.492) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

Its inclination of 4.92° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 44.4 km/s at perihelion and falls to 15.1 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 = 22.18 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

The current orbit solution is based on 49 observations and has a weighted RMS residual of 0.3292 arcseconds.

Condition code U = 2 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
1.32 AU
Eccentricity
0.492
Perihelion
0.671 AU
Aphelion
1.96944 AU
Inclination
4.92°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
254.54°

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
2026-Dec-18 16:31 0.249605 AU
37340418 km
10.66 km/s
2030-Jan-23 06:51 0.053065 AU
7938415 km
13.12 km/s
2033-Feb-03 15:14 0.163407 AU
24445337 km
19.57 km/s
2036-Feb-14 01:33 0.364802 AU
54573676 km
25.65 km/s
2052-Jul-07 18:24 0.425554 AU
63661917 km
27.13 km/s
2055-Jul-18 11:01 0.223202 AU
33390584 km
21.17 km/s
2058-Jul-28 11:59 0.025690 AU
3843168 km
15.39 km/s
2061-Aug-09 03:06 0.135478 AU
20267238 km
10.81 km/s
2064-Sep-12 13:54 0.266567 AU
39877869 km
11.10 km/s
2067-Jul-14 12:50 0.473575 AU
70845789 km
7.92 km/s
2067-Oct-11 03:50 0.320045 AU
47877997 km
13.76 km/s
2070-Nov-03 16:10 0.329702 AU
49322708 km
14.41 km/s
2073-Nov-28 15:10 0.299037 AU
44735296 km
12.86 km/s
2074-Jan-31 01:41 0.399972 AU
59834919 km
6.43 km/s
2077-Jan-02 06:42 0.207870 AU
31096869 km
9.52 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
22.18

Orbit Quality

RMS
0.32923
Condition
2
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.

Keep exploring

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