View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38107U 26145.52761845 +.00000000 +00000-0 +00000-0 0 00008
2 38107 0.0417 111.6384 0002442 315.0964 82.8244 1.00271433 06
| Epoch (UTC): | 25 May 2026 12:39:46 |
| Eccentricity: | 0.0002442 |
| inclination: | 0.0417° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 111.6384° |
| argument of perigee: | 315.0964° |
| revolutions per day: | 1.00271433 |
| mean anomaly at epoch: | 82.8244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|