SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 YL1

2017 YL1

2017 YL1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.129 AU it takes 1.20 yr to circle the Sun.

Apollo Observations: 47
Orbital Period · P
1.20 yr
v(q)
45.6 km/s
v(Q)
17.3 km/s
Diameter · ≈
0.04 km
TJ
5.43
Eccentricity · e
0.4504

Orbit and dynamics

Between its closest point (0.62 AU) and its farthest (1.638 AU), the heliocentric distance changes by 1.018 AU over every revolution.

One full revolution takes 1.20 yr (438 days), computed from the semi-major axis of 1.129 AU.

The high eccentricity (0.45) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 9.42° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 45.6 km/s at perihelion and falls to 17.3 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 = 24.81 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 47 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5958 arcseconds.

Condition code U = 8 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
1.129 AU
Eccentricity
0.4504
Perihelion
0.62 AU
Aphelion
1.637502 AU
Inclination
9.42°
Orbital Period
— yr
Epoch
2458108.5
Mean Anomaly
50.69°

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
2029-Dec-14 17:05 0.004685 AU
700870 km
12.00 km/s
2035-Dec-13 19:06 0.001876 AU
280717 km
11.12 km/s
2040-May-30 21:17 0.058989 AU
8824622 km
12.41 km/s
2041-Dec-11 21:11 0.021415 AU
3203661 km
10.26 km/s
2046-May-29 13:49 0.058328 AU
8725782 km
13.22 km/s
2047-Dec-10 23:05 0.095525 AU
14290394 km
9.44 km/s
2052-May-27 14:23 0.058192 AU
8705423 km
13.94 km/s
2053-Dec-09 05:56 0.148879 AU
22271997 km
8.83 km/s
2058-May-26 01:02 0.059138 AU
8846993 km
14.99 km/s
2064-May-22 20:30 0.064160 AU
9598273 km
16.49 km/s
2065-Nov-03 22:09 0.296977 AU
44427080 km
10.73 km/s
2065-Dec-25 01:36 0.304973 AU
45623329 km
8.44 km/s
2070-May-19 21:45 0.123255 AU
18438633 km
18.52 km/s
2071-Oct-21 17:58 0.346955 AU
51903763 km
12.61 km/s
2072-Jan-05 02:30 0.383030 AU
57300447 km
9.30 km/s
2076-May-15 21:00 0.209632 AU
31360520 km
20.70 km/s
2077-Oct-09 13:41 0.370362 AU
55405300 km
14.07 km/s
2078-Jan-12 22:07 0.434200 AU
64955409 km
10.07 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
24.81

Orbit Quality

RMS
0.59578
Condition
8
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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