View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 55611U 26145.37785958 +.00000000 +00000-0 +20693-4 0 00005
2 55611 43.0027 281.4780 0001671 261.5139 98.5524 15.27577137 06
| Epoch (UTC): | 25 May 2026 09:04:07 |
| Eccentricity: | 0.0001671 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 281.4780° |
| argument of perigee: | 261.5139° |
| revolutions per day: | 15.27577137 |
| mean anomaly at epoch: | 98.5524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|