View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11574U 26021.51127997 +.00000000 +00000-0 +20640-3 0 00008
2 11574 74.0680 178.3679 0015774 358.5371 1.5736 14.42315012 07
| Epoch (UTC): | 21 January 2026 12:16:14 |
| Eccentricity: | 0.0015774 |
| inclination: | 74.0680° |
| perigee height: | 740 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 178.3679° |
| argument of perigee: | 358.5371° |
| revolutions per day: | 14.42315012 |
| mean anomaly at epoch: | 1.5736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|