View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59584U 26145.46835881 +.00000000 +00000-0 +12973-4 0 00001
2 59584 43.0035 295.5066 0001542 276.6927 83.3749 15.27575725 02
| Epoch (UTC): | 25 May 2026 11:14:26 |
| Eccentricity: | 0.0001542 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.5066° |
| argument of perigee: | 276.6927° |
| revolutions per day: | 15.27575725 |
| mean anomaly at epoch: | 83.3749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|