View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22081U 26109.20846956 +.00000000 +00000-0 +80161-4 0 00004
2 22081 74.0418 295.5916 0035641 195.0605 164.9490 14.34845388 02
| Epoch (UTC): | 19 April 2026 05:00:11 |
| Eccentricity: | 0.0035641 |
| inclination: | 74.0418° |
| perigee height: | 750 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 295.5916° |
| argument of perigee: | 195.0605° |
| revolutions per day: | 14.34845388 |
| mean anomaly at epoch: | 164.9490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|