View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68955U 26145.58335647 +.00000000 +00000-0 -22928-1 0 00000
2 68955 53.1594 268.0883 0001100 55.1423 40.1021 15.63565237 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001100 |
| inclination: | 53.1594° |
| perigee height: | 377 km |
| apogee height: | 378 km |
| right ascension of ascending node: | 268.0883° |
| argument of perigee: | 55.1423° |
| revolutions per day: | 15.63565237 |
| mean anomaly at epoch: | 40.1021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|