SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FP127

2017 FP127

2017 FP127 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.181 AU it takes 1.28 yr to circle the Sun.

Apollo Observations: 25
Orbital Period · P
1.28 yr
v(q)
33.7 km/s
v(Q)
22.3 km/s
Diameter · ≈
0.01 km
TJ
5.34
Eccentricity · e
0.2025

Orbit and dynamics

The path is an ellipse reaching 0.942 AU from the Sun at perihelion and 1.42 AU at aphelion, a radial span of 0.478 AU.

Applying Kepler's third law to a = 1.181 AU gives an orbital period of 1.28 yr, or about 469 days.

An eccentricity of 0.203 makes the orbit moderately elongated.

Its inclination of 2.58° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 33.7 km/s at perihelion and falls to 22.3 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 = 28.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.01 km.

Observation record and orbit quality

The current orbit solution is based on 25 observations and has a weighted RMS residual of 0.7544 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
1.181 AU
Eccentricity
0.2025
Perihelion
0.942 AU
Aphelion
1.420153 AU
Inclination
2.58°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
100.36°

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
2030-Aug-12 18:32 0.401169 AU
60013980 km
7.02 km/s
2034-Dec-09 00:44 0.043225 AU
6466312 km
6.33 km/s
2039-Aug-29 08:49 0.379267 AU
56737592 km
6.75 km/s
2043-Nov-25 11:53 0.273777 AU
40956390 km
13.02 km/s
2044-Jun-15 16:29 0.328961 AU
49211817 km
5.62 km/s
2048-Sep-20 14:11 0.329872 AU
49348103 km
5.90 km/s
2049-Apr-13 22:16 0.283241 AU
42372283 km
13.19 km/s
2053-Jul-09 20:19 0.380527 AU
56925998 km
6.60 km/s
2057-Oct-22 04:01 0.213478 AU
31935899 km
4.06 km/s
2058-Mar-30 19:14 0.022296 AU
3335466 km
6.50 km/s
2062-Jul-28 18:11 0.404644 AU
60533831 km
7.01 km/s
2071-Aug-12 14:29 0.400824 AU
59962471 km
7.02 km/s
2075-Dec-08 03:51 0.044237 AU
6617710 km
6.77 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
28.4

Orbit Quality

RMS
0.75439
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.

Keep exploring

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