View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57081U 26145.65998017 +.00000000 +00000-0 +52030-4 0 00001
2 57081 43.0053 21.2918 0001417 266.4705 93.5985 15.27578199 07
| Epoch (UTC): | 25 May 2026 15:50:22 |
| Eccentricity: | 0.0001417 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.2918° |
| argument of perigee: | 266.4705° |
| revolutions per day: | 15.27578199 |
| mean anomaly at epoch: | 93.5985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|