SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 QO1

2017 QO1

2017 QO1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.897 AU and a period of 0.85 yr.

Aten Observations: 16
Orbital Period · P
0.85 yr
v(q)
38.1 km/s
v(Q)
25.9 km/s
Diameter · ≈
0.01 km
TJ
6.61
Eccentricity · e
0.1902

Orbit and dynamics

The path is an ellipse reaching 0.727 AU from the Sun at perihelion and 1.068 AU at aphelion, a radial span of 0.341 AU.

Applying Kepler's third law to a = 0.897 AU gives an orbital period of 0.85 yr, or about 311 days.

An eccentricity of 0.19 makes the orbit moderately elongated.

Its inclination of 2.24° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 38.1 km/s at perihelion and falls to 25.9 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 = 27 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 16 observations and has a weighted RMS residual of 0.7535 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
0.8975 AU
Eccentricity
0.1902
Perihelion
0.727 AU
Aphelion
1.068204 AU
Inclination
2.24°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
350.12°

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
2028-Jun-05 10:45 0.100549 AU
15041885 km
8.22 km/s
2028-Dec-11 07:59 0.230055 AU
34415764 km
6.77 km/s
2040-Feb-22 11:26 0.233995 AU
35005156 km
6.93 km/s
2040-Sep-01 08:19 0.115477 AU
17275127 km
8.55 km/s
2045-Jun-11 02:00 0.244455 AU
36569990 km
13.80 km/s
2046-Aug-25 03:51 0.271752 AU
40653465 km
15.12 km/s
2051-Jun-04 22:07 0.049397 AU
7389663 km
8.03 km/s
2063-Sep-01 03:30 0.011580 AU
1732383 km
4.83 km/s
2068-Jun-11 19:04 0.155216 AU
23220030 km
13.77 km/s
2069-Aug-23 18:20 0.191911 AU
28709454 km
15.87 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
27.0

Orbit Quality

RMS
0.75351
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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