SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FT90

2017 FT90

2017 FT90 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.124 AU it takes 1.19 yr to circle the Sun.

Apollo Observations: 43
Orbital Period · P
1.19 yr
v(q)
35.2 km/s
v(Q)
22.4 km/s
Diameter · ≈
0.02 km
TJ
5.51
Eccentricity · e
0.2231

Orbit and dynamics

Between its closest point (0.874 AU) and its farthest (1.375 AU), the heliocentric distance changes by 0.501 AU over every revolution.

One full revolution takes 1.19 yr (435 days), computed from the semi-major axis of 1.124 AU.

An eccentricity of 0.223 makes the orbit moderately elongated.

The orbital plane is tilted 12.62° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 35.2 km/s at perihelion and falls to 22.4 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 = 26.2 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.02 km.

Observation record and orbit quality

Astrometry from 43 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5396 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
1.124 AU
Eccentricity
0.2231
Perihelion
0.874 AU
Aphelion
1.374764 AU
Inclination
12.62°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
318.33°

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
2028-Oct-07 21:33 0.073658 AU
11019087 km
10.24 km/s
2034-Sep-29 21:40 0.180531 AU
27007097 km
16.87 km/s
2036-Apr-07 13:36 0.282414 AU
42248577 km
20.32 km/s
2042-Mar-27 05:53 0.035045 AU
5242675 km
13.24 km/s
2048-Mar-16 13:59 0.035959 AU
5379329 km
7.67 km/s
2053-Oct-07 22:25 0.080540 AU
12048601 km
7.52 km/s
2059-Oct-05 07:58 0.098995 AU
14809485 km
13.13 km/s
2065-Sep-24 03:27 0.413284 AU
61826442 km
20.61 km/s
2066-Jul-16 10:49 0.426832 AU
63853143 km
7.08 km/s
2067-Apr-02 00:51 0.271691 AU
40644410 km
16.47 km/s
2072-Aug-21 04:56 0.346871 AU
51891108 km
7.21 km/s
2073-Mar-20 15:04 0.031579 AU
4724098 km
9.59 km/s
2079-Mar-16 17:39 0.156577 AU
23423621 km
6.56 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
26.2

Orbit Quality

RMS
0.53957
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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