SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 SR2

2016 SR2

2016 SR2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.061 AU it takes 1.09 yr to circle the Sun.

Apollo Observations: 86
Orbital Period · P
1.09 yr
v(q)
35.6 km/s
v(Q)
23.5 km/s
Diameter · ≈
0.02 km
TJ
5.79
Eccentricity · e
0.2054

Orbit and dynamics

The path is an ellipse reaching 0.843 AU from the Sun at perihelion and 1.279 AU at aphelion, a radial span of 0.436 AU.

Applying Kepler's third law to a = 1.061 AU gives an orbital period of 1.09 yr, or about 399 days.

An eccentricity of 0.205 makes the orbit moderately elongated.

Its inclination of 4.07° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 35.6 km/s at perihelion and falls to 23.5 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 = 26.2 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 86 observations and has a weighted RMS residual of 0.3364 arcseconds.

Condition code U = 1 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
1.061 AU
Eccentricity
0.2054
Perihelion
0.843 AU
Aphelion
1.278929 AU
Inclination
4.07°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
241.42°

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-Sep-16 19:47 0.408046 AU
61042768 km
17.82 km/s
2028-Sep-08 21:53 0.170700 AU
25536419 km
3.74 km/s
2028-Dec-01 02:45 0.138652 AU
20742030 km
4.87 km/s
2029-May-31 04:40 0.248738 AU
37210690 km
5.39 km/s
2030-Apr-06 12:42 0.231132 AU
34576898 km
12.63 km/s
2039-Sep-27 02:06 0.199392 AU
29828691 km
11.67 km/s
2040-Jul-26 05:46 0.257997 AU
38595784 km
5.48 km/s
2041-Feb-09 10:28 0.128624 AU
19241932 km
4.39 km/s
2041-Apr-10 20:56 0.144665 AU
21641600 km
3.37 km/s
2042-Apr-16 12:05 0.438506 AU
65599600 km
18.75 km/s
2051-Oct-06 18:00 0.017302 AU
2588271 km
6.46 km/s
2052-Jul-04 00:17 0.269436 AU
40307079 km
5.76 km/s
2053-Mar-26 16:41 0.018193 AU
2721661 km
5.54 km/s
2054-Apr-21 04:04 0.498333 AU
74549577 km
20.52 km/s
2064-Oct-04 16:55 0.017706 AU
2648757 km
6.48 km/s
2065-Jul-11 02:55 0.259026 AU
38749687 km
5.62 km/s
2066-Mar-13 10:02 0.097890 AU
14644107 km
3.56 km/s
2067-Apr-17 10:06 0.376460 AU
56317612 km
16.94 km/s
2078-Oct-03 02:55 0.045201 AU
6761959 km
7.39 km/s
2079-Jul-18 16:53 0.252688 AU
37801559 km
5.51 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
26.2

Orbit Quality

RMS
0.33638
Condition
1
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.