View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66888U 26145.58335647 +.00000000 +00000-0 +17612-2 0 00007
2 66888 53.1588 27.0588 0001110 99.0060 350.6347 15.30167728 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001110 |
| inclination: | 53.1588° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 27.0588° |
| argument of perigee: | 99.0060° |
| revolutions per day: | 15.30167728 |
| mean anomaly at epoch: | 350.6347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|