View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20465U 26162.51020962 +.00000000 +00000-0 +19828-3 0 00003
2 20465 82.4661 314.9538 0009952 20.7009 339.4622 15.11973969 02
| Epoch (UTC): | 11 June 2026 12:14:42 |
| Eccentricity: | 0.0009952 |
| inclination: | 82.4661° |
| perigee height: | 523 km |
| apogee height: | 537 km |
| right ascension of ascending node: | 314.9538° |
| argument of perigee: | 20.7009° |
| revolutions per day: | 15.11973969 |
| mean anomaly at epoch: | 339.4622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|