View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55458U 26145.27970764 +.00000000 +00000-0 +32430-5 0 00007
2 55458 43.0013 256.3386 0001089 273.6454 86.4273 15.27576360 04
| Epoch (UTC): | 25 May 2026 06:42:46 |
| Eccentricity: | 0.0001089 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.3386° |
| argument of perigee: | 273.6454° |
| revolutions per day: | 15.27576360 |
| mean anomaly at epoch: | 86.4273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|