SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 CQ1

2017 CQ1

2017 CQ1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.184 AU it takes 1.29 yr to circle the Sun.

Apollo Observations: 52
Orbital Period · P
1.29 yr
v(q)
34 km/s
v(Q)
22 km/s
Diameter · ≈
0.05 km
TJ
5.32
Eccentricity · e
0.2148

Orbit and dynamics

Between its closest point (0.93 AU) and its farthest (1.438 AU), the heliocentric distance changes by 0.508 AU over every revolution.

One full revolution takes 1.29 yr (471 days), computed from the semi-major axis of 1.184 AU.

An eccentricity of 0.215 makes the orbit moderately elongated.

The orbital plane is tilted 7.84° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 34 km/s at perihelion and falls to 22 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 = 24.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

Astrometry from 52 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4491 arcseconds.

Condition code U = 6 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
1.184 AU
Eccentricity
0.2148
Perihelion
0.93 AU
Aphelion
1.438323 AU
Inclination
7.84°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
27.38°

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
2030-Nov-06 06:37 0.474842 AU
71035372 km
8.02 km/s
2035-Jul-10 13:43 0.067556 AU
10106278 km
4.90 km/s
2039-Oct-30 20:46 0.469656 AU
70259578 km
7.95 km/s
2044-Jul-14 01:48 0.059497 AU
8900566 km
6.46 km/s
2053-Jul-18 00:50 0.058724 AU
8785060 km
8.43 km/s
2057-Feb-10 20:57 0.293773 AU
43947798 km
20.00 km/s
2062-Jul-24 02:17 0.054250 AU
8115632 km
11.82 km/s
2066-Feb-16 19:25 0.139597 AU
20883468 km
16.08 km/s
2071-Jul-30 15:44 0.131931 AU
19736606 km
15.76 km/s
2075-Feb-22 22:16 0.075890 AU
11352961 km
11.93 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
24.3

Orbit Quality

RMS
0.44911
Condition
6
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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