View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25406U 26022.27286718 +.00000000 +00000-0 -86375-4 0 00007
2 25406 70.7457 227.1534 0006468 224.9313 135.1284 14.12485261 09
| Epoch (UTC): | 22 January 2026 06:32:55 |
| Eccentricity: | 0.0006468 |
| inclination: | 70.7457° |
| perigee height: | 846 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 227.1534° |
| argument of perigee: | 224.9313° |
| revolutions per day: | 14.12485261 |
| mean anomaly at epoch: | 135.1284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|