View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28647U 26160.31139587 +.00000000 +00000-0 +28582-3 0 00000
2 28647 56.9952 211.5597 0053478 185.5392 174.5080 15.46228667 07
| Epoch (UTC): | 09 June 2026 07:28:24 |
| Eccentricity: | 0.0053478 |
| inclination: | 56.9952° |
| perigee height: | 391 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 211.5597° |
| argument of perigee: | 185.5392° |
| revolutions per day: | 15.46228667 |
| mean anomaly at epoch: | 174.5080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|