View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66341U 26145.45962272 +.00000000 +00000-0 +57639-3 0 00001
2 66341 43.0005 139.1032 0001479 272.8966 87.1716 15.27593532 06
| Epoch (UTC): | 25 May 2026 11:01:51 |
| Eccentricity: | 0.0001479 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.1032° |
| argument of perigee: | 272.8966° |
| revolutions per day: | 15.27593532 |
| mean anomaly at epoch: | 87.1716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|