SpaceAtlas Space Object Data
NASA JPL SBDB · 2017 FT102

2017 FT102

2017 FT102 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.038 AU it takes 1.06 yr to circle the Sun.

Apollo Observations: 79
Orbital Period · P
1.06 yr
v(q)
31 km/s
v(Q)
27.6 km/s
Diameter · ≈
0 km
TJ
5.91
Eccentricity · e
0.0589

Orbit and dynamics

The path is an ellipse reaching 0.977 AU from the Sun at perihelion and 1.099 AU at aphelion, a radial span of 0.122 AU.

Applying Kepler's third law to a = 1.038 AU gives an orbital period of 1.06 yr, or about 386 days.

With e = 0.059, the orbit is close to circular.

Its inclination of 1.52° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 31 km/s at perihelion and falls to 27.6 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 = 29.5 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0 km.

Observation record and orbit quality

The current orbit solution is based on 79 observations and has a weighted RMS residual of 0.4262 arcseconds.

Condition code U = 3 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
1.038 AU
Eccentricity
0.0589
Perihelion
0.977 AU
Aphelion
1.099138 AU
Inclination
1.52°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
196.41°

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
2034-Mar-10 11:22 0.441260 AU
66011616 km
15.17 km/s
2035-Mar-25 15:17 0.078264 AU
11708139 km
4.40 km/s
2035-Nov-28 05:04 0.112956 AU
16897956 km
2.63 km/s
2036-Aug-21 14:46 0.122989 AU
18398854 km
5.60 km/s
2037-Sep-05 00:17 0.470817 AU
70433281 km
15.82 km/s
2053-Mar-15 19:52 0.304930 AU
45616867 km
11.13 km/s
2054-May-10 01:16 0.038034 AU
5689773 km
1.62 km/s
2054-Sep-29 12:46 0.080262 AU
12007000 km
1.84 km/s
2055-Aug-24 02:21 0.273724 AU
40948508 km
10.03 km/s
2071-Mar-13 05:28 0.288902 AU
43219138 km
10.94 km/s
2072-Sep-11 19:08 0.062122 AU
9293260 km
1.52 km/s
2073-Aug-21 07:06 0.291321 AU
43580966 km
10.71 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
29.5

Orbit Quality

RMS
0.42619
Condition
3
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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