View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 19548U 26145.44502751 +.00000000 +00000-0 +00000-0 0 00006
2 19548 12.6191 341.1577 0039339 357.8555 15.0924 1.00264374 00
| Epoch (UTC): | 25 May 2026 10:40:50 |
| Eccentricity: | 0.0039339 |
| inclination: | 12.6191° |
| perigee height: | 35623 km |
| apogee height: | 35955 km |
| right ascension of ascending node: | 341.1577° |
| argument of perigee: | 357.8555° |
| revolutions per day: | 1.00264374 |
| mean anomaly at epoch: | 15.0924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|