View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22889U 26129.31787882 +.00000000 +00000-0 +47232-4 0 00008
2 22889 82.9466 60.4189 0050846 121.4051 239.2094 13.78275077 07
| Epoch (UTC): | 09 May 2026 07:37:44 |
| Eccentricity: | 0.0050846 |
| inclination: | 82.9466° |
| perigee height: | 933 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 60.4189° |
| argument of perigee: | 121.4051° |
| revolutions per day: | 13.78275077 |
| mean anomaly at epoch: | 239.2094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|