View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56827U 26145.03170485 +.00000000 +00000-0 +51528-5 0 00003
2 56827 43.0040 35.9159 0001277 254.7961 105.2750 15.27580340 09
| Epoch (UTC): | 25 May 2026 00:45:39 |
| Eccentricity: | 0.0001277 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.9159° |
| argument of perigee: | 254.7961° |
| revolutions per day: | 15.27580340 |
| mean anomaly at epoch: | 105.2750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|