View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56038U 26145.53307394 +.00000000 +00000-0 +26757-4 0 00008
2 56038 43.0020 331.5884 0001076 265.2376 94.8353 15.27576198 03
| Epoch (UTC): | 25 May 2026 12:47:37 |
| Eccentricity: | 0.0001076 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.5884° |
| argument of perigee: | 265.2376° |
| revolutions per day: | 15.27576198 |
| mean anomaly at epoch: | 94.8353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|