View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56014U 26145.23940933 +.00000000 +00000-0 +10539-3 0 00001
2 56014 43.0049 332.8487 0001924 279.6333 80.4301 15.27589560 06
| Epoch (UTC): | 25 May 2026 05:44:44 |
| Eccentricity: | 0.0001924 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 332.8487° |
| argument of perigee: | 279.6333° |
| revolutions per day: | 15.27589560 |
| mean anomaly at epoch: | 80.4301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|