View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 61978U 26145.19953970 +.00000000 +00000-0 +33019-3 0 00004
2 61978 43.0012 107.5191 0000897 270.8780 89.1969 15.27583215 04
| Epoch (UTC): | 25 May 2026 04:47:20 |
| Eccentricity: | 0.0000897 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.5191° |
| argument of perigee: | 270.8780° |
| revolutions per day: | 15.27583215 |
| mean anomaly at epoch: | 89.1969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|