View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66212U 26145.61726286 +.00000000 +00000-0 +42046-3 0 00005
2 66212 53.1600 232.8637 0000649 79.2838 280.8236 15.30207912 00
| Epoch (UTC): | 25 May 2026 14:48:51 |
| Eccentricity: | 0.0000649 |
| inclination: | 53.1600° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.8637° |
| argument of perigee: | 79.2838° |
| revolutions per day: | 15.30207912 |
| mean anomaly at epoch: | 280.8236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|