View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55491U 26145.63957007 +.00000000 +00000-0 -42625-6 0 00008
2 55491 43.0006 246.8287 0000961 266.1037 93.9704 15.27573380 00
| Epoch (UTC): | 25 May 2026 15:20:58 |
| Eccentricity: | 0.0000961 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 246.8287° |
| argument of perigee: | 266.1037° |
| revolutions per day: | 15.27573380 |
| mean anomaly at epoch: | 93.9704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|