SpaceAtlas Space Object Data
NASA JPL SBDB · 2019 ST9

2019 ST9

2019 ST9 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.667 AU it takes 2.15 yr to circle the Sun.

Apollo Observations: 100
Orbital Period · P
2.15 yr
v(q)
46.6 km/s
v(Q)
11.4 km/s
Diameter · ≈
0.27 km
TJ
3.9
Eccentricity · e
0.6067

Orbit and dynamics

Between its closest point (0.656 AU) and its farthest (2.678 AU), the heliocentric distance changes by 2.022 AU over every revolution.

One full revolution takes 2.15 yr (786 days), computed from the semi-major axis of 1.667 AU.

The high eccentricity (0.607) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

A steep inclination of 29.85° carries it well above and below the ecliptic plane.

By the vis-viva equation its orbital speed rises to 46.6 km/s at perihelion and falls to 11.4 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 = 20.61 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.27 km.

Observation record and orbit quality

Astrometry from 100 individual observations underpins this orbit; the fit leaves an RMS residual of 0.4158 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
1.667 AU
Eccentricity
0.6067
Perihelion
0.656 AU
Aphelion
2.678369 AU
Inclination
29.85°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
350.9°

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
2032-Oct-17 06:32 0.267930 AU
40081810 km
25.85 km/s
2035-Mar-06 04:44 0.362074 AU
54165530 km
19.72 km/s
2047-Oct-27 12:21 0.341507 AU
51088758 km
17.36 km/s
2050-Apr-12 15:00 0.133901 AU
20031292 km
24.15 km/s
2060-Oct-13 20:24 0.334337 AU
50016141 km
28.29 km/s
2063-Feb-21 23:07 0.422414 AU
63192244 km
19.92 km/s
2065-May-07 07:24 0.473282 AU
70801920 km
34.07 km/s
2075-Oct-27 00:21 0.291486 AU
43605705 km
18.48 km/s
2078-Apr-07 17:19 0.130681 AU
19549548 km
22.87 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
20.61

Orbit Quality

RMS
0.41575
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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