View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56170U 26144.97315692 +.00000000 +00000-0 +19580-3 0 00007
2 56170 81.0014 101.6742 0010373 10.1966 349.9412 14.08863171 04
| Epoch (UTC): | 24 May 2026 23:21:20 |
| Eccentricity: | 0.0010373 |
| inclination: | 81.0014° |
| perigee height: | 856 km |
| apogee height: | 871 km |
| right ascension of ascending node: | 101.6742° |
| argument of perigee: | 10.1966° |
| revolutions per day: | 14.08863171 |
| mean anomaly at epoch: | 349.9412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|