View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 46469U 26145.60981457 +.00000000 +00000-0 -46171-4 0 00004
2 46469 65.9974 271.4956 0009741 239.0277 120.9835 13.83372174 03
| Epoch (UTC): | 25 May 2026 14:38:07 |
| Eccentricity: | 0.0009741 |
| inclination: | 65.9974° |
| perigee height: | 945 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 271.4956° |
| argument of perigee: | 239.0277° |
| revolutions per day: | 13.83372174 |
| mean anomaly at epoch: | 120.9835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|