View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56354U 26145.45653509 +.00000000 +00000-0 +21587-4 0 00008
2 56354 97.4447 146.4473 0002018 89.7799 270.3660 15.05648325 02
| Epoch (UTC): | 25 May 2026 10:57:24 |
| Eccentricity: | 0.0002018 |
| inclination: | 97.4447° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.4473° |
| argument of perigee: | 89.7799° |
| revolutions per day: | 15.05648325 |
| mean anomaly at epoch: | 270.3660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|