View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45685U 26145.34466928 +.00000000 +00000-0 +11341-2 0 00003
2 45685 53.0421 15.0662 0006461 129.9764 230.1815 15.56202004 05
| Epoch (UTC): | 25 May 2026 08:16:19 |
| Eccentricity: | 0.0006461 |
| inclination: | 53.0421° |
| perigee height: | 394 km |
| apogee height: | 403 km |
| right ascension of ascending node: | 15.0662° |
| argument of perigee: | 129.9764° |
| revolutions per day: | 15.56202004 |
| mean anomaly at epoch: | 230.1815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|