View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55808U 26145.42428273 +.00000000 +00000-0 +34344-3 0 00000
2 55808 87.9149 309.5168 0001424 92.8432 267.2864 13.19727107 00
| Epoch (UTC): | 25 May 2026 10:10:58 |
| Eccentricity: | 0.0001424 |
| inclination: | 87.9149° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5168° |
| argument of perigee: | 92.8432° |
| revolutions per day: | 13.19727107 |
| mean anomaly at epoch: | 267.2864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|