View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59409U 26145.49590685 +.00000000 +00000-0 +49000-4 0 00001
2 59409 42.9988 331.9060 0000741 279.9056 80.1712 15.27581448 05
| Epoch (UTC): | 25 May 2026 11:54:06 |
| Eccentricity: | 0.0000741 |
| inclination: | 42.9988° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.9060° |
| argument of perigee: | 279.9056° |
| revolutions per day: | 15.27581448 |
| mean anomaly at epoch: | 80.1712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|