View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22676U 26070.78076903 +.00000000 +00000-0 +66662-4 0 00001
2 22676 74.0398 105.1131 0017001 69.9136 290.3845 14.35263735 01
| Epoch (UTC): | 11 March 2026 18:44:18 |
| Eccentricity: | 0.0017001 |
| inclination: | 74.0398° |
| perigee height: | 762 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 105.1131° |
| argument of perigee: | 69.9136° |
| revolutions per day: | 14.35263735 |
| mean anomaly at epoch: | 290.3845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|