View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 45438U 26145.39485944 +.00000000 +00000-0 -11359-2 0 00003
2 45438 87.8909 25.6017 0001787 81.8098 278.3233 13.11417261 00
| Epoch (UTC): | 25 May 2026 09:28:35 |
| Eccentricity: | 0.0001787 |
| inclination: | 87.8909° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6017° |
| argument of perigee: | 81.8098° |
| revolutions per day: | 13.11417261 |
| mean anomaly at epoch: | 278.3233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|