View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56115U 26145.54849176 +.00000000 +00000-0 +10228-3 0 00009
2 56115 43.0112 84.2861 0003314 267.5955 92.4518 15.27599122 02
| Epoch (UTC): | 25 May 2026 13:09:49 |
| Eccentricity: | 0.0003314 |
| inclination: | 43.0112° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 84.2861° |
| argument of perigee: | 267.5955° |
| revolutions per day: | 15.27599122 |
| mean anomaly at epoch: | 92.4518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|