View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55831U 26145.36625309 +.00000000 +00000-0 +40250-6 0 00004
2 55831 87.9175 278.9849 0002085 104.9577 255.1788 13.20771069 08
| Epoch (UTC): | 25 May 2026 08:47:24 |
| Eccentricity: | 0.0002085 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9849° |
| argument of perigee: | 104.9577° |
| revolutions per day: | 13.20771069 |
| mean anomaly at epoch: | 255.1788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|