View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46032U 26145.37562882 +.00000000 +00000-0 +28725-4 0 00005
2 46032 53.1578 130.4963 0001157 84.1938 275.9195 15.30192370 08
| Epoch (UTC): | 25 May 2026 09:00:54 |
| Eccentricity: | 0.0001157 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 130.4963° |
| argument of perigee: | 84.1938° |
| revolutions per day: | 15.30192370 |
| mean anomaly at epoch: | 275.9195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|