View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54778U 26145.42899927 +.00000000 +00000-0 +55462-3 0 00007
2 54778 53.2113 44.6895 0001459 104.2395 255.8759 15.08792647 07
| Epoch (UTC): | 25 May 2026 10:17:45 |
| Eccentricity: | 0.0001459 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.6895° |
| argument of perigee: | 104.2395° |
| revolutions per day: | 15.08792647 |
| mean anomaly at epoch: | 255.8759° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|