View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56383U 26145.42810133 +.00000000 +00000-0 +42125-4 0 00006
2 56383 43.0022 124.7044 0001352 262.6725 97.3973 15.27581172 08
| Epoch (UTC): | 25 May 2026 10:16:27 |
| Eccentricity: | 0.0001352 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.7044° |
| argument of perigee: | 262.6725° |
| revolutions per day: | 15.27581172 |
| mean anomaly at epoch: | 97.3973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|