View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57222U 26145.48350053 +.00000000 +00000-0 +41171-4 0 00005
2 57222 43.0018 316.7278 0001397 255.5081 104.5616 15.27577396 01
| Epoch (UTC): | 25 May 2026 11:36:14 |
| Eccentricity: | 0.0001397 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.7278° |
| argument of perigee: | 255.5081° |
| revolutions per day: | 15.27577396 |
| mean anomaly at epoch: | 104.5616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|