SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 XR61

2017 XR61

2017 XR61 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.274 AU it takes 1.44 yr to circle the Sun.

Apollo Observations: 50
Orbital Period · P
1.44 yr
v(q)
37 km/s
v(Q)
18.8 km/s
Diameter · ≈
0.09 km
TJ
5.02
Eccentricity · e
0.3259

Orbit and dynamics

The path is an ellipse reaching 0.859 AU from the Sun at perihelion and 1.689 AU at aphelion, a radial span of 0.83 AU.

Applying Kepler's third law to a = 1.274 AU gives an orbital period of 1.44 yr, or about 525 days.

An eccentricity of 0.326 makes the orbit moderately elongated.

Its inclination of 4.52° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37 km/s at perihelion and falls to 18.8 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 = 23.1 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.09 km.

Observation record and orbit quality

The current orbit solution is based on 50 observations and has a weighted RMS residual of 0.4841 arcseconds.

Condition code U = 4 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
1.274 AU
Eccentricity
0.3259
Perihelion
0.859 AU
Aphelion
1.689197 AU
Inclination
4.52°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
269.96°

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
2027-Dec-15 11:10 0.357758 AU
53519843 km
5.63 km/s
2028-Apr-21 18:40 0.138627 AU
20738276 km
6.51 km/s
2030-Dec-24 17:04 0.430231 AU
64361631 km
21.54 km/s
2038-Jun-15 15:47 0.247954 AU
37093352 km
15.76 km/s
2041-Jan-15 22:26 0.024455 AU
3658474 km
9.22 km/s
2041-Jul-22 02:50 0.457328 AU
68415259 km
7.41 km/s
2051-Mar-17 20:45 0.153444 AU
22954910 km
7.11 km/s
2060-Nov-30 15:52 0.429172 AU
64203175 km
7.15 km/s
2061-May-26 15:21 0.060511 AU
9052258 km
7.43 km/s
2063-Dec-27 19:57 0.370287 AU
55394221 km
19.78 km/s
2071-Jun-11 08:21 0.152746 AU
22850536 km
12.97 km/s
2074-Jan-06 09:19 0.170831 AU
25555892 km
13.81 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
23.1

Orbit Quality

RMS
0.48409
Condition
4
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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