View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56908U 26145.28623067 +.00000000 +00000-0 +17390-4 0 00007
2 56908 43.0037 358.0146 0001089 264.6465 95.4262 15.27578323 06
| Epoch (UTC): | 25 May 2026 06:52:10 |
| Eccentricity: | 0.0001089 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 358.0146° |
| argument of perigee: | 264.6465° |
| revolutions per day: | 15.27578323 |
| mean anomaly at epoch: | 95.4262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|