View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22285U 26038.49264104 +.00000000 +00000-0 -46064-4 0 00006
2 22285 71.0201 67.6598 0005114 325.2803 34.7985 14.15441111 06
| Epoch (UTC): | 07 February 2026 11:49:24 |
| Eccentricity: | 0.0005114 |
| inclination: | 71.0201° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 67.6598° |
| argument of perigee: | 325.2803° |
| revolutions per day: | 14.15441111 |
| mean anomaly at epoch: | 34.7985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|