SpaceAtlas Space Object Data
NASA JPL SBDB · 2015 XR55

2015 XR55

2015 XR55 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.11 AU it takes 1.17 yr to circle the Sun.

Apollo Observations: 61
Orbital Period · P
1.17 yr
v(q)
45.8 km/s
v(Q)
17.5 km/s
Diameter · ≈
0.3 km
TJ
5.41
Eccentricity · e
0.4474

Orbit and dynamics

Between its closest point (0.613 AU) and its farthest (1.607 AU), the heliocentric distance changes by 0.994 AU over every revolution.

One full revolution takes 1.17 yr (427 days), computed from the semi-major axis of 1.11 AU.

The high eccentricity (0.447) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 28.83° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 45.8 km/s at perihelion and falls to 17.5 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 = 20.37 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.3 km.

Observation record and orbit quality

Astrometry from 61 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4875 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
1.11 AU
Eccentricity
0.4474
Perihelion
0.613 AU
Aphelion
1.606614 AU
Inclination
28.83°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
154.44°

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
2029-Jun-04 07:51 0.423238 AU
63315552 km
23.64 km/s
2030-Oct-21 17:53 0.383548 AU
57377900 km
22.95 km/s
2035-Mar-06 06:03 0.492531 AU
73681615 km
25.12 km/s
2036-Jun-11 19:08 0.443237 AU
66307250 km
23.51 km/s
2037-Oct-23 06:53 0.427866 AU
64007876 km
24.88 km/s
2042-Mar-12 14:21 0.453821 AU
67890605 km
23.94 km/s
2043-Jun-20 06:03 0.462539 AU
69194851 km
23.17 km/s
2044-Oct-25 01:28 0.476646 AU
71305299 km
26.82 km/s
2049-Mar-19 07:36 0.421035 AU
62985905 km
23.10 km/s
2050-Jun-27 19:45 0.480438 AU
71872564 km
22.59 km/s
2050-Nov-06 21:24 0.479900 AU
71791985 km
16.32 km/s
2056-Mar-25 22:41 0.395551 AU
59173578 km
22.59 km/s
2057-Jul-05 10:37 0.495977 AU
74197054 km
21.73 km/s
2057-Nov-03 21:10 0.452717 AU
67725571 km
16.24 km/s
2063-Apr-02 15:01 0.375997 AU
56248298 km
22.33 km/s
2064-Nov-01 00:16 0.425606 AU
63669814 km
16.18 km/s
2070-Apr-09 00:55 0.362781 AU
54271267 km
22.28 km/s
2071-Oct-30 05:20 0.399611 AU
59781007 km
16.19 km/s
2077-Apr-15 07:06 0.355072 AU
53117959 km
22.36 km/s
2078-Oct-27 16:01 0.374834 AU
56074311 km
16.24 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
20.37

Orbit Quality

RMS
0.48752
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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