View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25774U 26067.54313400 +.00000000 +00000-0 +58820-4 0 00006
2 25774 51.5284 259.8645 0374040 242.9026 134.2426 13.46767277 06
| Epoch (UTC): | 08 March 2026 13:02:06 |
| Eccentricity: | 0.0374040 |
| inclination: | 51.5284° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 259.8645° |
| argument of perigee: | 242.9026° |
| revolutions per day: | 13.46767277 |
| mean anomaly at epoch: | 134.2426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|