View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 08924U 26044.47166199 +.00000000 +00000-0 +12192-3 0 00003
2 08924 74.0555 50.7864 0015353 246.2948 226.0700 14.38574571 05
| Epoch (UTC): | 13 February 2026 11:19:11 |
| Eccentricity: | 0.0015353 |
| inclination: | 74.0555° |
| perigee height: | 752 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 50.7864° |
| argument of perigee: | 246.2948° |
| revolutions per day: | 14.38574571 |
| mean anomaly at epoch: | 226.0700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|