View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68922U 26145.37134366 +.00000000 +00000-0 +47202-3 0 00009
2 68922 51.8741 178.3190 0021744 65.4462 294.8785 15.30209310 06
| Epoch (UTC): | 25 May 2026 08:54:44 |
| Eccentricity: | 0.0021744 |
| inclination: | 51.8741° |
| perigee height: | 460 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 178.3190° |
| argument of perigee: | 65.4462° |
| revolutions per day: | 15.30209310 |
| mean anomaly at epoch: | 294.8785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|