View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39090U 26066.47560920 +.00000000 +00000-0 +19693-3 0 00008
2 39090 98.3885 249.2224 0008883 168.1704 191.9693 14.37092860 01
| Epoch (UTC): | 07 March 2026 11:24:52 |
| Eccentricity: | 0.0008883 |
| inclination: | 98.3885° |
| perigee height: | 762 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 249.2224° |
| argument of perigee: | 168.1704° |
| revolutions per day: | 14.37092860 |
| mean anomaly at epoch: | 191.9693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|