View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58424U 26145.56157437 +.00000000 +00000-0 +42883-4 0 00001
2 58424 43.0033 338.2300 0001105 269.1044 90.9681 15.27577672 02
| Epoch (UTC): | 25 May 2026 13:28:40 |
| Eccentricity: | 0.0001105 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.2300° |
| argument of perigee: | 269.1044° |
| revolutions per day: | 15.27577672 |
| mean anomaly at epoch: | 90.9681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|