View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56706U 26145.48229206 +.00000000 +00000-0 +74143-4 0 00001
2 56706 43.0026 207.6649 0001566 264.4644 95.6028 15.26741405 08
| Epoch (UTC): | 25 May 2026 11:34:30 |
| Eccentricity: | 0.0001566 |
| inclination: | 43.0026° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 207.6649° |
| argument of perigee: | 264.4644° |
| revolutions per day: | 15.26741405 |
| mean anomaly at epoch: | 95.6028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|