View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55989U 26145.60809458 +.00000000 +00000-0 -10880-4 0 00009
2 55989 43.0042 345.1749 0001369 275.3587 84.7109 15.27586394 09
| Epoch (UTC): | 25 May 2026 14:35:39 |
| Eccentricity: | 0.0001369 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.1749° |
| argument of perigee: | 275.3587° |
| revolutions per day: | 15.27586394 |
| mean anomaly at epoch: | 84.7109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|