View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55609U 26145.42140624 +.00000000 +00000-0 +74959-5 0 00008
2 55609 43.0031 280.9622 0001388 269.2081 90.8612 15.27574337 05
| Epoch (UTC): | 25 May 2026 10:06:49 |
| Eccentricity: | 0.0001388 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.9622° |
| argument of perigee: | 269.2081° |
| revolutions per day: | 15.27574337 |
| mean anomaly at epoch: | 90.8612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|