View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25724U 26140.39800976 +.00000000 +00000-0 +10372-2 0 00003
2 25724 28.2245 50.0162 2131841 109.1239 275.1045 9.37508734 04
| Epoch (UTC): | 20 May 2026 09:33:08 |
| Eccentricity: | 0.2131841 |
| inclination: | 28.2245° |
| perigee height: | 1097 km |
| apogee height: | 5148 km |
| right ascension of ascending node: | 50.0162° |
| argument of perigee: | 109.1239° |
| revolutions per day: | 9.37508734 |
| mean anomaly at epoch: | 275.1045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|