View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25406U 26162.56554324 +.00000000 +00000-0 -13415-3 0 00009
2 25406 70.7313 289.8935 0007870 347.0950 12.9967 14.12423490 08
| Epoch (UTC): | 11 June 2026 13:34:22 |
| Eccentricity: | 0.0007870 |
| inclination: | 70.7313° |
| perigee height: | 845 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 289.8935° |
| argument of perigee: | 347.0950° |
| revolutions per day: | 14.12423490 |
| mean anomaly at epoch: | 12.9967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|