View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66594U 26145.58425979 +.00000000 +00000-0 +59288-3 0 00005
2 66594 43.0044 342.1128 0001768 259.4376 100.6277 15.27585042 08
| Epoch (UTC): | 25 May 2026 14:01:20 |
| Eccentricity: | 0.0001768 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1128° |
| argument of perigee: | 259.4376° |
| revolutions per day: | 15.27585042 |
| mean anomaly at epoch: | 100.6277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|