View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55361U 26145.57824422 +.00000000 +00000-0 +16029-4 0 00007
2 55361 43.0034 214.3701 0001879 274.9988 85.0649 15.27576631 01
| Epoch (UTC): | 25 May 2026 13:52:40 |
| Eccentricity: | 0.0001879 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 214.3701° |
| argument of perigee: | 274.9988° |
| revolutions per day: | 15.27576631 |
| mean anomaly at epoch: | 85.0649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|