View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66491U 26145.42699709 +.00000000 +00000-0 +23576-3 0 00009
2 66491 43.0010 277.4256 0001371 234.8043 125.2680 15.27586279 01
| Epoch (UTC): | 25 May 2026 10:14:52 |
| Eccentricity: | 0.0001371 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.4256° |
| argument of perigee: | 234.8043° |
| revolutions per day: | 15.27586279 |
| mean anomaly at epoch: | 125.2680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|