View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55457U 26145.58479928 +.00000000 +00000-0 +23804-4 0 00000
2 55457 43.0033 254.3302 0001285 271.7725 88.2980 15.27576450 04
| Epoch (UTC): | 25 May 2026 14:02:06 |
| Eccentricity: | 0.0001285 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.3302° |
| argument of perigee: | 271.7725° |
| revolutions per day: | 15.27576450 |
| mean anomaly at epoch: | 88.2980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|