View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59608U 26145.48815860 +.00000000 +00000-0 +61085-4 0 00003
2 59608 43.0015 320.2416 0001225 260.5728 99.4985 15.27576576 06
| Epoch (UTC): | 25 May 2026 11:42:56 |
| Eccentricity: | 0.0001225 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.2416° |
| argument of perigee: | 260.5728° |
| revolutions per day: | 15.27576576 |
| mean anomaly at epoch: | 99.4985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|