View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22195U 26144.37120935 +.00000000 +00000-0 +00000-0 0 00009
2 22195 52.6605 281.7119 0137772 176.8869 204.7538 6.47293592 02
| Epoch (UTC): | 24 May 2026 08:54:32 |
| Eccentricity: | 0.0137772 |
| inclination: | 52.6605° |
| perigee height: | 5616 km |
| apogee height: | 5951 km |
| right ascension of ascending node: | 281.7119° |
| argument of perigee: | 176.8869° |
| revolutions per day: | 6.47293592 |
| mean anomaly at epoch: | 204.7538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|