View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52266U 26145.34063839 +.00000000 +00000-0 +25880-4 0 00005
2 52266 53.2144 125.0198 0001162 85.9870 274.1255 15.08850777 09
| Epoch (UTC): | 25 May 2026 08:10:31 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.0198° |
| argument of perigee: | 85.9870° |
| revolutions per day: | 15.08850777 |
| mean anomaly at epoch: | 274.1255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|