View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59611U 26145.52799620 +.00000000 +00000-0 +52993-4 0 00005
2 59611 43.0018 320.5447 0001023 276.8508 83.2227 15.27570724 01
| Epoch (UTC): | 25 May 2026 12:40:18 |
| Eccentricity: | 0.0001023 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.5447° |
| argument of perigee: | 276.8508° |
| revolutions per day: | 15.27570724 |
| mean anomaly at epoch: | 83.2227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|