View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56123U 26145.51398249 +.00000000 +00000-0 +54954-4 0 00000
2 56123 43.0055 73.6184 0001223 273.8067 86.2645 15.27574478 07
| Epoch (UTC): | 25 May 2026 12:20:08 |
| Eccentricity: | 0.0001223 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.6184° |
| argument of perigee: | 273.8067° |
| revolutions per day: | 15.27574478 |
| mean anomaly at epoch: | 86.2645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|