View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58525U 26145.38983302 +.00000000 +00000-0 +21542-4 0 00000
2 58525 43.0019 30.0988 0001118 287.8254 72.2476 15.27583914 02
| Epoch (UTC): | 25 May 2026 09:21:21 |
| Eccentricity: | 0.0001118 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 30.0988° |
| argument of perigee: | 287.8254° |
| revolutions per day: | 15.27583914 |
| mean anomaly at epoch: | 72.2476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|