View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56921U 26144.94387861 +.00000000 +00000-0 +59258-4 0 00002
2 56921 43.0016 359.7384 0001416 265.9973 94.0717 15.27575912 03
| Epoch (UTC): | 24 May 2026 22:39:11 |
| Eccentricity: | 0.0001416 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 359.7384° |
| argument of perigee: | 265.9973° |
| revolutions per day: | 15.27575912 |
| mean anomaly at epoch: | 94.0717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|