View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55411U 26145.41642632 +.00000000 +00000-0 +39481-5 0 00005
2 55411 69.9993 231.1877 0002960 271.0648 89.0172 14.98331109 03
| Epoch (UTC): | 25 May 2026 09:59:39 |
| Eccentricity: | 0.0002960 |
| inclination: | 69.9993° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 231.1877° |
| argument of perigee: | 271.0648° |
| revolutions per day: | 14.98331109 |
| mean anomaly at epoch: | 89.0172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|