View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66419U 26145.32577514 +.00000000 +00000-0 +80987-4 0 00007
2 66419 50.0026 17.3387 0000926 64.9736 295.1232 13.29322617 02
| Epoch (UTC): | 25 May 2026 07:49:06 |
| Eccentricity: | 0.0000926 |
| inclination: | 50.0026° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.3387° |
| argument of perigee: | 64.9736° |
| revolutions per day: | 13.29322617 |
| mean anomaly at epoch: | 295.1232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|