SpaceAtlas Space Object Data
NASA JPL SBDB · 2009 SY

2009 SY

2009 SY belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.251 AU it takes 1.40 yr to circle the Sun.

Apollo Observations: 60
Orbital Period · P
1.40 yr
v(q)
42.8 km/s
v(Q)
16.6 km/s
Diameter · ≈
0.09 km
TJ
5.01
Eccentricity · e
0.4408

Orbit and dynamics

The path is an ellipse reaching 0.699 AU from the Sun at perihelion and 1.802 AU at aphelion, a radial span of 1.103 AU.

Applying Kepler's third law to a = 1.251 AU gives an orbital period of 1.40 yr, or about 511 days.

The high eccentricity (0.441) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 14.68° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 42.8 km/s at perihelion and falls to 16.6 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 = 22.99 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 60 observations and has a weighted RMS residual of 0.6056 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
1.251 AU
Eccentricity
0.4408
Perihelion
0.699 AU
Aphelion
1.802441 AU
Inclination
14.68°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
50.73°

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
2030-Aug-21 12:26 0.227558 AU
34042142 km
10.63 km/s
2033-Feb-05 15:00 0.310047 AU
46382400 km
23.24 km/s
2037-Aug-22 06:03 0.256591 AU
38385436 km
10.14 km/s
2040-Feb-04 00:19 0.352358 AU
52712062 km
24.56 km/s
2044-Jul-09 11:21 0.330538 AU
49447812 km
9.08 km/s
2044-Aug-26 15:42 0.315771 AU
47238609 km
9.75 km/s
2047-Jan-30 23:23 0.423882 AU
63411916 km
26.76 km/s
2051-Jun-19 19:15 0.357544 AU
53487800 km
11.67 km/s
2051-Sep-02 17:51 0.374939 AU
56090062 km
9.93 km/s
2054-Jan-27 04:28 0.492688 AU
73705046 km
28.90 km/s
2058-Jun-03 14:00 0.369476 AU
55272852 km
13.27 km/s
2058-Sep-09 20:54 0.440344 AU
65874548 km
10.43 km/s
2065-May-19 21:11 0.366405 AU
54813425 km
14.11 km/s
2072-May-05 12:56 0.349967 AU
52354362 km
14.29 km/s
2079-Apr-22 03:14 0.320692 AU
47974787 km
13.92 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
22.99

Orbit Quality

RMS
0.60559
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

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