View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56037U 26145.46304123 +.00000000 +00000-0 +23155-4 0 00005
2 56037 43.0054 317.1742 0001736 274.9450 85.1203 15.27576545 08
| Epoch (UTC): | 25 May 2026 11:06:46 |
| Eccentricity: | 0.0001736 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.1742° |
| argument of perigee: | 274.9450° |
| revolutions per day: | 15.27576545 |
| mean anomaly at epoch: | 85.1203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|