View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22087U 26105.38030566 +.00000000 +00000-0 +00000-0 0 00007
2 22087 12.8589 24.5846 0005816 112.8067 71.5827 0.99202913 03
| Epoch (UTC): | 15 April 2026 09:07:38 |
| Eccentricity: | 0.0005816 |
| inclination: | 12.8589° |
| perigee height: | 36064 km |
| apogee height: | 36114 km |
| right ascension of ascending node: | 24.5846° |
| argument of perigee: | 112.8067° |
| revolutions per day: | 0.99202913 |
| mean anomaly at epoch: | 71.5827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|