View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22220U 26021.48704336 +.00000000 +00000-0 -22808-4 0 00002
2 22220 71.0006 287.8061 0012556 177.9148 354.5447 14.16850628 05
| Epoch (UTC): | 21 January 2026 11:41:20 |
| Eccentricity: | 0.0012556 |
| inclination: | 71.0006° |
| perigee height: | 827 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 287.8061° |
| argument of perigee: | 177.9148° |
| revolutions per day: | 14.16850628 |
| mean anomaly at epoch: | 354.5447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|