View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22889U 26041.33198203 +.00000000 +00000-0 +44336-4 0 00008
2 22889 82.9470 125.9531 0049750 10.9302 349.2924 13.78272249 05
| Epoch (UTC): | 10 February 2026 07:58:03 |
| Eccentricity: | 0.0049750 |
| inclination: | 82.9470° |
| perigee height: | 933 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 125.9531° |
| argument of perigee: | 10.9302° |
| revolutions per day: | 13.78272249 |
| mean anomaly at epoch: | 349.2924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|