View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59441U 26144.74621441 +.00000000 +00000-0 -33660-4 0 00005
2 59441 53.1612 288.4197 0001198 87.6772 272.4366 15.30200045 08
| Epoch (UTC): | 24 May 2026 17:54:32 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.4197° |
| argument of perigee: | 87.6772° |
| revolutions per day: | 15.30200045 |
| mean anomaly at epoch: | 272.4366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|