View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66211U 26145.49918627 +.00000000 +00000-0 +50830-3 0 00002
2 66211 53.1608 232.8360 0000784 30.4450 329.6597 15.30210040 07
| Epoch (UTC): | 25 May 2026 11:58:49 |
| Eccentricity: | 0.0000784 |
| inclination: | 53.1608° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.8360° |
| argument of perigee: | 30.4450° |
| revolutions per day: | 15.30210040 |
| mean anomaly at epoch: | 329.6597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|