SpaceAtlas Space Object Data
NASA JPL SBDB · 2009 SL2

2009 SL2

2009 SL2 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.046 AU it takes 1.07 yr to circle the Sun.

Apollo Observations: 56
Orbital Period · P
1.07 yr
v(q)
37.5 km/s
v(Q)
22.6 km/s
Diameter · ≈
0.12 km
TJ
5.77
Eccentricity · e
0.249

Orbit and dynamics

Between its closest point (0.786 AU) and its farthest (1.306 AU), the heliocentric distance changes by 0.52 AU over every revolution.

One full revolution takes 1.07 yr (391 days), computed from the semi-major axis of 1.046 AU.

An eccentricity of 0.249 makes the orbit moderately elongated.

A steep inclination of 23.74° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 37.5 km/s at perihelion and falls to 22.6 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 = 22.3 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

Astrometry from 56 individual observations underpins this orbit; the fit leaves an RMS residual of 0.7008 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
1.046 AU
Eccentricity
0.249
Perihelion
0.786 AU
Aphelion
1.306454 AU
Inclination
23.74°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
320.41°

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
2037-Feb-20 10:21 0.304814 AU
45599528 km
19.36 km/s
2038-Mar-31 22:45 0.194414 AU
29083881 km
14.68 km/s
2038-Oct-19 02:32 0.411601 AU
61574682 km
12.29 km/s
2039-Sep-21 19:44 0.194163 AU
29046399 km
12.67 km/s
2040-Sep-15 06:09 0.302849 AU
45305579 km
18.29 km/s
2052-Feb-14 12:08 0.384511 AU
57521978 km
21.37 km/s
2053-Mar-21 17:28 0.157226 AU
23520667 km
14.98 km/s
2053-Oct-27 00:32 0.449985 AU
67316787 km
12.03 km/s
2054-May-19 14:01 0.390900 AU
58477853 km
13.49 km/s
2054-Sep-26 04:42 0.239770 AU
35869071 km
12.46 km/s
2055-Sep-15 05:52 0.235959 AU
35298901 km
16.43 km/s
2067-Feb-08 19:46 0.457828 AU
68490030 km
23.34 km/s
2068-Mar-13 06:48 0.154083 AU
23050439 km
15.57 km/s
2068-Nov-04 12:10 0.479443 AU
71723647 km
11.57 km/s
2069-May-04 04:04 0.345839 AU
51736756 km
14.39 km/s
2069-Sep-30 22:12 0.285817 AU
42757681 km
12.40 km/s
2070-Sep-15 04:02 0.186137 AU
27845646 km
14.97 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
22.3

Orbit Quality

RMS
0.70082
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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