View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66424U 26145.54165914 +.00000000 +00000-0 +52006-3 0 00004
2 66424 43.0025 200.4368 0001700 253.6339 106.4326 15.27581899 07
| Epoch (UTC): | 25 May 2026 12:59:59 |
| Eccentricity: | 0.0001700 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.4368° |
| argument of perigee: | 253.6339° |
| revolutions per day: | 15.27581899 |
| mean anomaly at epoch: | 106.4326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|