View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56481U 26145.40875560 +.00000000 +00000-0 -10294-3 0 00000
2 56481 69.9986 290.9117 0003028 267.8278 92.2534 14.98321459 06
| Epoch (UTC): | 25 May 2026 09:48:36 |
| Eccentricity: | 0.0003028 |
| inclination: | 69.9986° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 290.9117° |
| argument of perigee: | 267.8278° |
| revolutions per day: | 14.98321459 |
| mean anomaly at epoch: | 92.2534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|