View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 54826U 26145.13321066 +.00000000 +00000-0 +26040-5 0 00005
2 54826 43.0010 64.4085 0000946 250.5455 109.5294 15.27575295 05
| Epoch (UTC): | 25 May 2026 03:11:49 |
| Eccentricity: | 0.0000946 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.4085° |
| argument of perigee: | 250.5455° |
| revolutions per day: | 15.27575295 |
| mean anomaly at epoch: | 109.5294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|