View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64209U 26145.40600810 +.00000000 +00000-0 +56546-3 0 00000
2 64209 53.1571 43.1071 0000916 62.9920 297.1174 15.30210622 08
| Epoch (UTC): | 25 May 2026 09:44:39 |
| Eccentricity: | 0.0000916 |
| inclination: | 53.1571° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.1071° |
| argument of perigee: | 62.9920° |
| revolutions per day: | 15.30210622 |
| mean anomaly at epoch: | 297.1174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|