View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54685U 26145.60984468 +.00000000 +00000-0 +32131-3 0 00007
2 54685 97.6884 315.6215 0002525 170.8627 189.2663 15.35755700 03
| Epoch (UTC): | 25 May 2026 14:38:10 |
| Eccentricity: | 0.0002525 |
| inclination: | 97.6884° |
| perigee height: | 457 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 315.6215° |
| argument of perigee: | 170.8627° |
| revolutions per day: | 15.35755700 |
| mean anomaly at epoch: | 189.2663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|