View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59570U 26145.40682725 +.00000000 +00000-0 +48321-4 0 00003
2 59570 43.0003 295.9150 0000613 333.9751 26.1069 15.27578770 03
| Epoch (UTC): | 25 May 2026 09:45:49 |
| Eccentricity: | 0.0000613 |
| inclination: | 43.0003° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 295.9150° |
| argument of perigee: | 333.9751° |
| revolutions per day: | 15.27578770 |
| mean anomaly at epoch: | 26.1069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|