View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57094U 26145.34332603 +.00000000 +00000-0 -31204-4 0 00005
2 57094 43.0037 23.2062 0001191 277.0291 83.0425 15.27570219 00
| Epoch (UTC): | 25 May 2026 08:14:23 |
| Eccentricity: | 0.0001191 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 23.2062° |
| argument of perigee: | 277.0291° |
| revolutions per day: | 15.27570219 |
| mean anomaly at epoch: | 83.0425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|