View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66856U 26145.40488844 +.00000000 +00000-0 +63230-3 0 00009
2 66856 43.0016 270.6170 0001809 253.5170 106.5483 15.27603371 03
| Epoch (UTC): | 25 May 2026 09:43:02 |
| Eccentricity: | 0.0001809 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.6170° |
| argument of perigee: | 253.5170° |
| revolutions per day: | 15.27603371 |
| mean anomaly at epoch: | 106.5483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|