View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25991U 26140.97866434 +.00000000 +00000-0 +60884-4 0 00009
2 25991 98.9979 179.1912 0011124 81.4896 339.7146 14.17552426 04
| Epoch (UTC): | 20 May 2026 23:29:16 |
| Eccentricity: | 0.0011124 |
| inclination: | 98.9979° |
| perigee height: | 826 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 179.1912° |
| argument of perigee: | 81.4896° |
| revolutions per day: | 14.17552426 |
| mean anomaly at epoch: | 339.7146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|