View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53619U 26145.31994743 +.00000000 +00000-0 +21926-4 0 00009
2 53619 53.2150 250.1053 0001393 94.7524 265.3627 15.08836338 01
| Epoch (UTC): | 25 May 2026 07:40:43 |
| Eccentricity: | 0.0001393 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 250.1053° |
| argument of perigee: | 94.7524° |
| revolutions per day: | 15.08836338 |
| mean anomaly at epoch: | 265.3627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|