View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22889U 26041.62236308 +.00000000 +00000-0 +42787-4 0 00007
2 22889 82.9470 125.7370 0049728 10.1195 350.0952 13.78272258 02
| Epoch (UTC): | 10 February 2026 14:56:12 |
| Eccentricity: | 0.0049728 |
| inclination: | 82.9470° |
| perigee height: | 933 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 125.7370° |
| argument of perigee: | 10.1195° |
| revolutions per day: | 13.78272258 |
| mean anomaly at epoch: | 350.0952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|