View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 58366U 26144.77825670 +.00000000 +00000-0 +45680-5 0 00008
2 58366 43.0019 280.9408 0001444 263.2901 96.7787 15.27568296 09
| Epoch (UTC): | 24 May 2026 18:40:41 |
| Eccentricity: | 0.0001444 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.9408° |
| argument of perigee: | 263.2901° |
| revolutions per day: | 15.27568296 |
| mean anomaly at epoch: | 96.7787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|