SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 SF9

2019 SF9

2019 SF9 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.056 AU it takes 1.09 yr to circle the Sun.

Apollo Observations: 91
Orbital Period · P
1.09 yr
v(q)
31.9 km/s
v(Q)
26.3 km/s
Diameter · ≈
0.05 km
TJ
5.73
Eccentricity · e
0.0952

Orbit and dynamics

The path is an ellipse reaching 0.956 AU from the Sun at perihelion and 1.157 AU at aphelion, a radial span of 0.201 AU.

Applying Kepler's third law to a = 1.056 AU gives an orbital period of 1.09 yr, or about 396 days.

With e = 0.095, the orbit is close to circular.

A steep inclination of 27.25° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 31.9 km/s at perihelion and falls to 26.3 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 = 24.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.05 km.

Observation record and orbit quality

The current orbit solution is based on 91 observations and has a weighted RMS residual of 0.2832 arcseconds.

Condition code U = 7 signals a poorly constrained orbit, so its future path should be treated as provisional.

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
1.056 AU
Eccentricity
0.0952
Perihelion
0.956 AU
Aphelion
1.156531 AU
Inclination
27.25°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
4.75°

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
2031-Sep-14 17:38 0.276972 AU
41434479 km
19.26 km/s
2032-Mar-31 15:52 0.312987 AU
46822196 km
15.46 km/s
2032-Oct-02 18:18 0.063247 AU
9461606 km
14.31 km/s
2033-Mar-23 17:08 0.101981 AU
15256079 km
14.48 km/s
2044-Sep-20 20:36 0.051694 AU
7733315 km
16.22 km/s
2045-Mar-27 05:41 0.161212 AU
24116987 km
14.20 km/s
2045-Oct-07 22:42 0.165127 AU
24702649 km
15.93 km/s
2046-Mar-24 16:04 0.149352 AU
22342764 km
16.55 km/s
2057-Sep-27 06:37 0.007038 AU
1052855 km
14.44 km/s
2058-Mar-25 00:24 0.095854 AU
14339585 km
13.75 km/s
2058-Oct-11 16:28 0.324111 AU
48486379 km
18.44 km/s
2059-Mar-27 00:32 0.293377 AU
43888570 km
19.29 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
24.4

Orbit Quality

RMS
0.2832
Condition
7
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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