View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 11574U 26088.16606742 +.00000000 +00000-0 +13629-3 0 00001
2 11574 74.0687 54.9870 0016751 225.1631 134.8166 14.42363023 02
| Epoch (UTC): | 29 March 2026 03:59:08 |
| Eccentricity: | 0.0016751 |
| inclination: | 74.0687° |
| perigee height: | 739 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 54.9870° |
| argument of perigee: | 225.1631° |
| revolutions per day: | 14.42363023 |
| mean anomaly at epoch: | 134.8166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|