View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66866U 26144.81769512 +.00000000 +00000-0 +53527-3 0 00006
2 66866 43.0029 273.9474 0002634 260.0730 99.9824 15.27593973 03
| Epoch (UTC): | 24 May 2026 19:37:28 |
| Eccentricity: | 0.0002634 |
| inclination: | 43.0029° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 273.9474° |
| argument of perigee: | 260.0730° |
| revolutions per day: | 15.27593973 |
| mean anomaly at epoch: | 99.9824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|