View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22219U 26039.09378858 +.00000000 +00000-0 -39731-4 0 00005
2 22219 71.0584 79.9415 0020354 247.7617 112.1346 14.14076578 07
| Epoch (UTC): | 08 February 2026 02:15:03 |
| Eccentricity: | 0.0020354 |
| inclination: | 71.0584° |
| perigee height: | 831 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 79.9415° |
| argument of perigee: | 247.7617° |
| revolutions per day: | 14.14076578 |
| mean anomaly at epoch: | 112.1346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|