SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FP101

2017 FP101

2017 FP101 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.087 AU it takes 1.13 yr to circle the Sun.

Apollo Observations: 49
Orbital Period · P
1.13 yr
v(q)
32.5 km/s
v(Q)
25.1 km/s
Diameter · ≈
0.04 km
TJ
5.69
Eccentricity · e
0.1278

Orbit and dynamics

Between its closest point (0.948 AU) and its farthest (1.226 AU), the heliocentric distance changes by 0.278 AU over every revolution.

One full revolution takes 1.13 yr (414 days), computed from the semi-major axis of 1.087 AU.

An eccentricity of 0.128 makes the orbit moderately elongated.

The orbital plane is tilted 6.62° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 32.5 km/s at perihelion and falls to 25.1 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 = 24.7 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.04 km.

Observation record and orbit quality

Astrometry from 49 individual observations underpins this orbit; the fit leaves an RMS residual of 0.3578 arcseconds.

Condition code U = 6 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
1.087 AU
Eccentricity
0.1278
Perihelion
0.948 AU
Aphelion
1.225919 AU
Inclination
6.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
119.34°

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
2033-Oct-24 00:18 0.038413 AU
5746511 km
4.59 km/s
2034-Apr-15 06:57 0.126919 AU
18986765 km
3.89 km/s
2043-Mar-16 15:45 0.066175 AU
9899705 km
7.77 km/s
2050-Oct-18 17:12 0.066613 AU
9965196 km
9.77 km/s
2052-Mar-28 12:24 0.318492 AU
47645717 km
17.05 km/s
2067-Oct-10 04:43 0.207788 AU
31084597 km
15.28 km/s
2069-Mar-20 07:21 0.088570 AU
13249921 km
11.53 km/s
2076-Oct-22 15:50 0.040231 AU
6018406 km
6.19 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
24.7

Orbit Quality

RMS
0.35783
Condition
6
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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