View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66114U 26145.12686626 +.00000000 +00000-0 +10789-2 0 00003
2 66114 53.1591 44.5640 0001109 87.2416 272.8712 15.30208117 03
| Epoch (UTC): | 25 May 2026 03:02:41 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.5640° |
| argument of perigee: | 87.2416° |
| revolutions per day: | 15.30208117 |
| mean anomaly at epoch: | 272.8712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|