View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59564U 26145.37872425 +.00000000 +00000-0 +23325-5 0 00008
2 59564 43.0040 285.3200 0001222 266.3098 93.7614 15.27577180 06
| Epoch (UTC): | 25 May 2026 09:05:21 |
| Eccentricity: | 0.0001222 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 285.3200° |
| argument of perigee: | 266.3098° |
| revolutions per day: | 15.27577180 |
| mean anomaly at epoch: | 93.7614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|