View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56411U 26145.40381778 +.00000000 +00000-0 +88422-4 0 00004
2 56411 43.0037 114.0801 0001254 275.7597 84.3112 15.27597025 07
| Epoch (UTC): | 25 May 2026 09:41:29 |
| Eccentricity: | 0.0001254 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.0801° |
| argument of perigee: | 275.7597° |
| revolutions per day: | 15.27597025 |
| mean anomaly at epoch: | 84.3112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|