View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58779U 26145.34379513 +.00000000 +00000-0 -39623-4 0 00000
2 58779 53.1614 17.8105 0001171 105.9789 254.1340 15.30207542 07
| Epoch (UTC): | 25 May 2026 08:15:03 |
| Eccentricity: | 0.0001171 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 17.8105° |
| argument of perigee: | 105.9789° |
| revolutions per day: | 15.30207542 |
| mean anomaly at epoch: | 254.1340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|