View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20443U 26156.44012455 +.00000000 +00000-0 +99816-4 0 00008
2 20443 98.2964 214.4209 0008947 304.8596 55.1751 14.39921042 07
| Epoch (UTC): | 05 June 2026 10:33:46 |
| Eccentricity: | 0.0008947 |
| inclination: | 98.2964° |
| perigee height: | 752 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 214.4209° |
| argument of perigee: | 304.8596° |
| revolutions per day: | 14.39921042 |
| mean anomaly at epoch: | 55.1751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|