View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22566U 26067.86112884 +.00000000 +00000-0 +10907-3 0 00003
2 22566 71.0071 216.9207 0011722 315.3400 44.6778 14.15308473 07
| Epoch (UTC): | 08 March 2026 20:40:01 |
| Eccentricity: | 0.0011722 |
| inclination: | 71.0071° |
| perigee height: | 833 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 216.9207° |
| argument of perigee: | 315.3400° |
| revolutions per day: | 14.15308473 |
| mean anomaly at epoch: | 44.6778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|