View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 06080U 26070.27371844 +.00000000 +00000-0 +24512-4 0 00006
2 06080 81.2421 166.8947 0048347 339.4650 20.4571 14.01290107 05
| Epoch (UTC): | 11 March 2026 06:34:09 |
| Eccentricity: | 0.0048347 |
| inclination: | 81.2421° |
| perigee height: | 854 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 166.8947° |
| argument of perigee: | 339.4650° |
| revolutions per day: | 14.01290107 |
| mean anomaly at epoch: | 20.4571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|