View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55463U 26145.34549205 +.00000000 +00000-0 +10809-2 0 00006
2 55463 43.0002 261.9477 0004063 315.4383 44.6138 15.16743631 03
| Epoch (UTC): | 25 May 2026 08:17:30 |
| Eccentricity: | 0.0004063 |
| inclination: | 43.0002° |
| perigee height: | 513 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 261.9477° |
| argument of perigee: | 315.4383° |
| revolutions per day: | 15.16743631 |
| mean anomaly at epoch: | 44.6138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|