View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57450U 26145.46660442 +.00000000 +00000-0 +94653-4 0 00005
2 57450 43.0038 175.2824 0001467 275.3450 84.7235 15.27561304 07
| Epoch (UTC): | 25 May 2026 11:11:54 |
| Eccentricity: | 0.0001467 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.2824° |
| argument of perigee: | 275.3450° |
| revolutions per day: | 15.27561304 |
| mean anomaly at epoch: | 84.7235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|