View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63474U 26145.42547484 +.00000000 +00000-0 +56226-3 0 00007
2 63474 43.0004 186.3041 0002333 240.0147 120.0473 15.27597748 01
| Epoch (UTC): | 25 May 2026 10:12:41 |
| Eccentricity: | 0.0002333 |
| inclination: | 43.0004° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 186.3041° |
| argument of perigee: | 240.0147° |
| revolutions per day: | 15.27597748 |
| mean anomaly at epoch: | 120.0473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|