View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59676U 26145.51939731 +.00000000 +00000-0 +22745-3 0 00005
2 59676 42.9988 327.8899 0001362 280.1497 79.9201 15.27581914 05
| Epoch (UTC): | 25 May 2026 12:27:55 |
| Eccentricity: | 0.0001362 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.8899° |
| argument of perigee: | 280.1497° |
| revolutions per day: | 15.27581914 |
| mean anomaly at epoch: | 79.9201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|