View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59549U 26144.69834906 +.00000000 +00000-0 +13318-3 0 00006
2 59549 43.0012 273.8608 0000950 278.0606 82.0138 15.27567651 08
| Epoch (UTC): | 24 May 2026 16:45:37 |
| Eccentricity: | 0.0000950 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.8608° |
| argument of perigee: | 278.0606° |
| revolutions per day: | 15.27567651 |
| mean anomaly at epoch: | 82.0138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|