View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55801U 26145.33260234 +.00000000 +00000-0 +28003-3 0 00009
2 55801 87.9167 279.0124 0002304 98.2558 261.8836 13.20773018 06
| Epoch (UTC): | 25 May 2026 07:58:56 |
| Eccentricity: | 0.0002304 |
| inclination: | 87.9167° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 279.0124° |
| argument of perigee: | 98.2558° |
| revolutions per day: | 13.20773018 |
| mean anomaly at epoch: | 261.8836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|