SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 RS2

2017 RS2

2017 RS2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.263 AU it takes 1.42 yr to circle the Sun.

Apollo Observations: 80
Orbital Period · P
1.42 yr
v(q)
32.6 km/s
v(Q)
21.5 km/s
Diameter · ≈
0.02 km
TJ
5.08
Eccentricity · e
0.204

Orbit and dynamics

The path is an ellipse reaching 1.006 AU from the Sun at perihelion and 1.521 AU at aphelion, a radial span of 0.515 AU.

Applying Kepler's third law to a = 1.263 AU gives an orbital period of 1.42 yr, or about 518 days.

An eccentricity of 0.204 makes the orbit moderately elongated.

Its inclination of 2.99° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 32.6 km/s at perihelion and falls to 21.5 km/s at aphelion.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 26.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

The current orbit solution is based on 80 observations and has a weighted RMS residual of 0.4741 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
1.263 AU
Eccentricity
0.204
Perihelion
1.006 AU
Aphelion
1.520652 AU
Inclination
2.99°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
70.4°

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-Jun-22 02:55 0.255089 AU
38160765 km
11.89 km/s
2027-Nov-28 20:29 0.324152 AU
48492479 km
4.88 km/s
2034-May-09 15:03 0.287174 AU
42960681 km
4.20 km/s
2034-Oct-06 00:37 0.186436 AU
27890486 km
10.66 km/s
2038-Jan-04 20:26 0.458995 AU
68664624 km
7.60 km/s
2051-Apr-20 05:57 0.375757 AU
56212489 km
5.85 km/s
2051-Oct-14 22:17 0.374103 AU
55964997 km
15.32 km/s
2054-Dec-26 18:15 0.436998 AU
65373963 km
7.00 km/s
2068-Apr-28 12:11 0.314116 AU
46991049 km
5.13 km/s
2068-Oct-10 09:29 0.234067 AU
35015894 km
12.90 km/s
2072-Jan-06 22:53 0.449665 AU
67268983 km
7.57 km/s
2075-Mar-21 11:01 0.458945 AU
68657243 km
7.75 km/s
2078-Jun-24 04:09 0.153351 AU
22940976 km
10.95 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
26.4

Orbit Quality

RMS
0.47407
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.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.