View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53470U 26145.39980866 +.00000000 +00000-0 -19409-3 0 00006
2 53470 97.4472 265.3275 0001992 132.7578 227.3817 15.05645393 09
| Epoch (UTC): | 25 May 2026 09:35:43 |
| Eccentricity: | 0.0001992 |
| inclination: | 97.4472° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 265.3275° |
| argument of perigee: | 132.7578° |
| revolutions per day: | 15.05645393 |
| mean anomaly at epoch: | 227.3817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|