View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57823U 26145.43410847 +.00000000 +00000-0 +31737-5 0 00003
2 57823 43.0009 55.3694 0001045 266.7162 93.3570 15.27581972 09
| Epoch (UTC): | 25 May 2026 10:25:06 |
| Eccentricity: | 0.0001045 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.3694° |
| argument of perigee: | 266.7162° |
| revolutions per day: | 15.27581972 |
| mean anomaly at epoch: | 93.3570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|