View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26906U 26071.96648632 +.00000000 +00000-0 +39406-3 0 00001
2 26906 63.4220 46.0408 0619880 341.5619 16.3801 13.45169688 05
| Epoch (UTC): | 12 March 2026 23:11:44 |
| Eccentricity: | 0.0619880 |
| inclination: | 63.4220° |
| perigee height: | 627 km |
| apogee height: | 1553 km |
| right ascension of ascending node: | 46.0408° |
| argument of perigee: | 341.5619° |
| revolutions per day: | 13.45169688 |
| mean anomaly at epoch: | 16.3801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|