View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54800U 26145.47079686 +.00000000 +00000-0 +11808-4 0 00007
2 54800 53.2148 49.2055 0001471 105.4908 254.6247 15.08843483 01
| Epoch (UTC): | 25 May 2026 11:17:56 |
| Eccentricity: | 0.0001471 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.2055° |
| argument of perigee: | 105.4908° |
| revolutions per day: | 15.08843483 |
| mean anomaly at epoch: | 254.6247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|