View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59582U 26145.46195421 +.00000000 +00000-0 +19309-2 0 00006
2 59582 43.0028 295.4591 0000652 280.7046 79.3732 15.27705571 04
| Epoch (UTC): | 25 May 2026 11:05:12 |
| Eccentricity: | 0.0000652 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 295.4591° |
| argument of perigee: | 280.7046° |
| revolutions per day: | 15.27705571 |
| mean anomaly at epoch: | 79.3732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|