View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66022U 26145.27925395 +.00000000 +00000-0 +45349-3 0 00007
2 66022 53.1585 108.0227 0001244 91.6998 268.4145 15.30195957 03
| Epoch (UTC): | 25 May 2026 06:42:07 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0227° |
| argument of perigee: | 91.6998° |
| revolutions per day: | 15.30195957 |
| mean anomaly at epoch: | 268.4145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|