View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63904U 26145.38085426 +.00000000 +00000-0 +47773-3 0 00000
2 63904 42.9992 103.3738 0001065 270.2275 89.8454 15.27586662 07
| Epoch (UTC): | 25 May 2026 09:08:25 |
| Eccentricity: | 0.0001065 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.3738° |
| argument of perigee: | 270.2275° |
| revolutions per day: | 15.27586662 |
| mean anomaly at epoch: | 89.8454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|