View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55484U 26144.74375330 +.00000000 +00000-0 +14273-4 0 00009
2 55484 43.0051 270.4812 0001599 278.5824 81.4847 15.27575466 05
| Epoch (UTC): | 24 May 2026 17:51:00 |
| Eccentricity: | 0.0001599 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.4812° |
| argument of perigee: | 278.5824° |
| revolutions per day: | 15.27575466 |
| mean anomaly at epoch: | 81.4847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|