SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 CP

2017 CP

2017 CP belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.132 AU it takes 1.20 yr to circle the Sun.

Apollo Observations: 27
Orbital Period · P
1.20 yr
v(q)
34.8 km/s
v(Q)
22.5 km/s
Diameter · ≈
0.01 km
TJ
5.51
Eccentricity · e
0.2138

Orbit and dynamics

The path is an ellipse reaching 0.89 AU from the Sun at perihelion and 1.374 AU at aphelion, a radial span of 0.484 AU.

Applying Kepler's third law to a = 1.132 AU gives an orbital period of 1.20 yr, or about 440 days.

An eccentricity of 0.214 makes the orbit moderately elongated.

Its inclination of 4.94° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 34.8 km/s at perihelion and falls to 22.5 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 = 27.2 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 27 observations and has a weighted RMS residual of 0.4477 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
1.132 AU
Eccentricity
0.2138
Perihelion
0.89 AU
Aphelion
1.374022 AU
Inclination
4.94°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
329.44°

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-18 01:00 0.331844 AU
49643173 km
6.43 km/s
2029-Feb-05 06:19 0.130684 AU
19550083 km
11.11 km/s
2034-Jun-03 17:28 0.362482 AU
54226541 km
6.77 km/s
2035-Feb-12 12:32 0.284804 AU
42606034 km
15.23 km/s
2039-Aug-15 22:40 0.432526 AU
64705016 km
18.96 km/s
2040-May-19 06:40 0.375525 AU
56177681 km
6.92 km/s
2041-Feb-19 00:59 0.446760 AU
66834305 km
19.51 km/s
2045-Aug-22 06:52 0.308779 AU
46192645 km
14.84 km/s
2046-May-04 23:05 0.368701 AU
55156953 km
6.82 km/s
2051-Aug-29 10:09 0.168278 AU
25174065 km
10.95 km/s
2052-Apr-19 17:43 0.343962 AU
51456039 km
6.47 km/s
2057-Sep-04 08:14 0.049016 AU
7332724 km
7.45 km/s
2058-Apr-06 00:01 0.304157 AU
45501269 km
5.92 km/s
2063-Sep-09 13:12 0.041423 AU
6196806 km
5.48 km/s
2064-Mar-26 10:54 0.273423 AU
40903506 km
5.47 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
27.2

Orbit Quality

RMS
0.44766
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.

Keep exploring

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