SpaceAtlas Space Object Data
NASA JPL SBDB · 2020 FT1

2020 FT1

2020 FT1 belongs to the Apollo group of near-Earth asteroids, whose orbits cross the path of Earth; with a semi-major axis of 1.104 AU it takes 1.16 yr to circle the Sun.

Apollo Observations: 63
Orbital Period · P
1.16 yr
v(q)
37.4 km/s
v(Q)
21.5 km/s
Diameter · ≈
0.12 km
TJ
5.6
Eccentricity · e
0.2705

Orbit and dynamics

Between its closest point (0.805 AU) and its farthest (1.403 AU), the heliocentric distance changes by 0.598 AU over every revolution.

One full revolution takes 1.16 yr (424 days), computed from the semi-major axis of 1.104 AU.

An eccentricity of 0.271 makes the orbit moderately elongated.

Its inclination of 4.79° keeps it close to the plane of the ecliptic.

By the vis-viva equation its orbital speed rises to 37.4 km/s at perihelion and falls to 21.5 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 = 22.4 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.12 km.

Observation record and orbit quality

Astrometry from 63 individual observations underpins this orbit; the fit leaves an RMS residual of 0.5354 arcseconds.

Condition code U = 4 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
1.104 AU
Eccentricity
0.2705
Perihelion
0.805 AU
Aphelion
1.402632 AU
Inclination
4.79°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
347.62°

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
2027-Apr-15 03:03 0.292276 AU
43723799 km
6.61 km/s
2027-Aug-11 11:45 0.213379 AU
31920982 km
8.00 km/s
2028-Jan-11 17:22 0.353517 AU
52885397 km
7.37 km/s
2034-May-28 16:23 0.105604 AU
15798079 km
5.96 km/s
2035-Feb-04 07:16 0.409725 AU
61293933 km
8.53 km/s
2035-Dec-01 23:42 0.317172 AU
47448200 km
17.89 km/s
2041-May-16 20:31 0.151759 AU
22702779 km
12.54 km/s
2042-Feb-23 08:28 0.419214 AU
62713518 km
8.77 km/s
2042-Nov-20 04:27 0.094694 AU
14165993 km
10.95 km/s
2048-May-07 19:15 0.348658 AU
52158518 km
18.57 km/s
2049-Mar-12 10:17 0.398227 AU
59573983 km
8.45 km/s
2049-Oct-25 05:21 0.121264 AU
18140811 km
6.20 km/s
2056-Apr-01 02:55 0.342646 AU
51259128 km
7.51 km/s
2056-Sep-03 16:34 0.207094 AU
30980866 km
8.11 km/s
2056-Dec-27 05:10 0.305239 AU
45663096 km
6.29 km/s
2063-Apr-28 23:36 0.242743 AU
36313784 km
5.66 km/s
2063-Jul-23 11:41 0.200545 AU
30001088 km
7.21 km/s
2064-Jan-20 19:08 0.379919 AU
56835006 km
7.93 km/s
2064-Dec-09 03:02 0.481739 AU
72067075 km
22.93 km/s
2070-May-26 15:09 0.079333 AU
11868029 km
7.03 km/s
2071-Feb-07 10:00 0.414795 AU
62052455 km
8.62 km/s
2071-Nov-30 21:43 0.289861 AU
43362520 km
17.04 km/s
2077-May-17 09:15 0.150801 AU
22559504 km
12.49 km/s
2078-Feb-23 06:17 0.420303 AU
62876424 km
8.76 km/s
2078-Nov-20 22:55 0.102622 AU
15352066 km
11.17 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
22.4

Orbit Quality

RMS
0.53545
Condition
4
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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