SpaceAtlas Space Object Data
NASA JPL SBDB · 2010 CE55

2010 CE55

2010 CE55 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.29 AU it takes 1.47 yr to circle the Sun.

Apollo Observations: 91
Orbital Period · P
1.47 yr
v(q)
32.8 km/s
v(Q)
21 km/s
Diameter · ≈
0.13 km
TJ
5
Eccentricity · e
0.2205

Orbit and dynamics

Between its closest point (1.005 AU) and its farthest (1.574 AU), the heliocentric distance changes by 0.569 AU over every revolution.

One full revolution takes 1.47 yr (535 days), computed from the semi-major axis of 1.29 AU.

An eccentricity of 0.221 makes the orbit moderately elongated.

Its inclination of 2.53° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.8 km/s at perihelion and falls to 21 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 22.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.13 km.

Observation record and orbit quality

Astrometry from 91 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5026 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
1.29 AU
Eccentricity
0.2205
Perihelion
1.005 AU
Aphelion
1.574445 AU
Inclination
2.53°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
325.08°

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
2029-Jan-29 13:42 0.453244 AU
67804270 km
6.98 km/s
2032-Jul-14 21:48 0.092800 AU
13882642 km
6.35 km/s
2035-Apr-13 11:49 0.226424 AU
33872611 km
10.80 km/s
2035-Sep-06 23:56 0.323603 AU
48410268 km
4.22 km/s
2038-Oct-18 02:48 0.492199 AU
73631954 km
7.62 km/s
2051-Feb-03 09:46 0.437880 AU
65505933 km
6.70 km/s
2051-Aug-09 12:33 0.470139 AU
70331791 km
17.76 km/s
2054-Jul-12 18:53 0.076247 AU
11406461 km
5.72 km/s
2057-Apr-13 20:16 0.219289 AU
32805190 km
10.58 km/s
2057-Sep-05 06:46 0.319194 AU
47750808 km
4.09 km/s
2060-Oct-14 19:09 0.482323 AU
72154564 km
7.43 km/s
2073-Jan-20 18:28 0.493527 AU
73830544 km
7.69 km/s
2076-Feb-27 22:10 0.338394 AU
50623029 km
4.61 km/s
2076-Jul-28 09:27 0.252871 AU
37828931 km
11.38 km/s
2079-May-01 21:00 0.040254 AU
6021850 km
4.93 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
22.2

Orbit Quality

RMS
0.50263
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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