View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22222U 26099.75144189 +.00000000 +00000-0 +13570-3 0 00007
2 22222 70.9968 229.6753 0215008 170.4700 190.0583 13.70708222 08
| Epoch (UTC): | 09 April 2026 18:02:04 |
| Eccentricity: | 0.0215008 |
| inclination: | 70.9968° |
| perigee height: | 838 km |
| apogee height: | 1156 km |
| right ascension of ascending node: | 229.6753° |
| argument of perigee: | 170.4700° |
| revolutions per day: | 13.70708222 |
| mean anomaly at epoch: | 190.0583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|