SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 BB30

2017 BB30

2017 BB30 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.981 AU and a period of 0.97 yr.

Aten Observations: 23
Orbital Period · P
0.97 yr
v(q)
36.4 km/s
v(Q)
24.8 km/s
Diameter · ≈
0.03 km
TJ
6.15
Eccentricity · e
0.1903

Orbit and dynamics

The path is an ellipse reaching 0.795 AU from the Sun at perihelion and 1.168 AU at aphelion, a radial span of 0.373 AU.

Applying Kepler's third law to a = 0.981 AU gives an orbital period of 0.97 yr, or about 355 days.

An eccentricity of 0.19 makes the orbit moderately elongated.

Its inclination of 2.98° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 36.4 km/s at perihelion and falls to 24.8 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 = 25.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.03 km.

Observation record and orbit quality

The current orbit solution is based on 23 observations and has a weighted RMS residual of 0.5746 arcseconds.

Condition code U = 5 indicates a moderately constrained orbit; predictions decades ahead still carry noticeable uncertainty.

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
0.9814 AU
Eccentricity
0.1903
Perihelion
0.795 AU
Aphelion
1.16816 AU
Inclination
2.98°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
135.21°

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
2045-Sep-22 08:18 0.381204 AU
57027346 km
18.00 km/s
2046-Sep-15 10:42 0.212968 AU
31859582 km
12.87 km/s
2047-Sep-08 18:26 0.052495 AU
7853162 km
7.78 km/s
2048-Sep-16 15:08 0.099410 AU
14871540 km
3.54 km/s
2049-Jun-25 03:15 0.194920 AU
29159599 km
6.25 km/s
2049-Nov-06 18:18 0.179339 AU
26828732 km
5.20 km/s
2050-May-21 05:13 0.218834 AU
32737076 km
7.03 km/s
2050-Dec-11 04:59 0.172171 AU
25756454 km
5.24 km/s
2051-Apr-15 16:48 0.194868 AU
29151799 km
6.05 km/s
2052-Jan-26 04:18 0.078690 AU
11771783 km
4.07 km/s
2053-Jan-31 16:17 0.065929 AU
9862889 km
8.43 km/s
2054-Jan-25 12:54 0.240685 AU
36006000 km
13.70 km/s
2055-Jan-18 19:33 0.413796 AU
61902962 km
18.98 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
25.2

Orbit Quality

RMS
0.57458
Condition
5
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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