View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66560U 26145.09025745 +.00000000 +00000-0 +74675-3 0 00008
2 66560 43.0026 275.6443 0003770 267.5154 92.5266 15.27593177 05
| Epoch (UTC): | 25 May 2026 02:09:58 |
| Eccentricity: | 0.0003770 |
| inclination: | 43.0026° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 275.6443° |
| argument of perigee: | 267.5154° |
| revolutions per day: | 15.27593177 |
| mean anomaly at epoch: | 92.5266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|