View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56162U 26145.61643052 +.00000000 +00000-0 +62806-4 0 00004
2 56162 81.0012 93.4174 0007229 30.5244 329.6331 13.84954536 05
| Epoch (UTC): | 25 May 2026 14:47:39 |
| Eccentricity: | 0.0007229 |
| inclination: | 81.0012° |
| perigee height: | 941 km |
| apogee height: | 952 km |
| right ascension of ascending node: | 93.4174° |
| argument of perigee: | 30.5244° |
| revolutions per day: | 13.84954536 |
| mean anomaly at epoch: | 329.6331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|