View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66538U 26145.45270957 +.00000000 +00000-0 +48819-3 0 00001
2 66538 43.0000 204.3861 0001168 273.5528 86.5190 15.27590251 05
| Epoch (UTC): | 25 May 2026 10:51:54 |
| Eccentricity: | 0.0001168 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3861° |
| argument of perigee: | 273.5528° |
| revolutions per day: | 15.27590251 |
| mean anomaly at epoch: | 86.5190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|