2016 TH56
Explore asteroids, comets and near-Earth objects with JPL orbital data.
Apollo
Observations: 63
Orbital Parameters
Semi-Major Axis
1.222 AU
Eccentricity
0.1891
Perihelion
0.991 AU
Aphelion
1.45308 AU
Inclination
13.7°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
322.97°
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 distance | Velocity |
|---|---|---|
| 2028-Aug-06 11:21 | 0.495469 AU 74121044 km |
8.20 km/s |
| 2032-Jul-02 23:26 | 0.488686 AU 73106364 km |
6.50 km/s |
| 2036-Apr-23 01:47 | 0.362483 AU 54226626 km |
6.57 km/s |
| 2039-Nov-18 17:14 | 0.244441 AU 36567809 km |
6.60 km/s |
| 2040-Mar-18 13:32 | 0.057901 AU 8661924 km |
7.72 km/s |
| 2043-Oct-14 05:16 | 0.302502 AU 45253715 km |
8.06 km/s |
| 2044-Mar-30 17:31 | 0.302479 AU 45250155 km |
13.96 km/s |
| 2047-Sep-17 20:37 | 0.398253 AU 59577743 km |
8.82 km/s |
| 2051-Aug-23 13:41 | 0.470437 AU 70376411 km |
8.69 km/s |
| 2059-Jun-17 08:10 | 0.464371 AU 69468864 km |
5.71 km/s |
| 2063-Mar-21 08:06 | 0.267514 AU 40019528 km |
7.95 km/s |
| 2066-Nov-06 12:26 | 0.249389 AU 37308045 km |
7.06 km/s |
| 2067-Mar-22 05:19 | 0.079535 AU 11898292 km |
8.90 km/s |
| 2070-Oct-05 02:24 | 0.335571 AU 50200750 km |
8.42 km/s |
| 2071-Apr-05 11:26 | 0.411556 AU 61567953 km |
16.77 km/s |
| 2074-Sep-08 06:05 | 0.430625 AU 64420527 km |
8.88 km/s |
| 2078-Aug-11 21:05 | 0.489982 AU 73300303 km |
8.39 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
22.2
Orbit Quality
RMS
0.57216
Condition
0
Orbit ID
—
