View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21903U 26073.52803271 +.00000000 +00000-0 +36792-4 0 00005
2 21903 82.9408 338.6865 0042217 192.6676 341.3748 13.74744218 01
| Epoch (UTC): | 14 March 2026 12:40:22 |
| Eccentricity: | 0.0042217 |
| inclination: | 82.9408° |
| perigee height: | 952 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 338.6865° |
| argument of perigee: | 192.6676° |
| revolutions per day: | 13.74744218 |
| mean anomaly at epoch: | 341.3748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|