View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52311U 26145.26890477 +.00000000 +00000-0 +22217-3 0 00003
2 52311 53.2121 105.3411 0001448 72.1503 287.9647 15.08844918 09
| Epoch (UTC): | 25 May 2026 06:27:13 |
| Eccentricity: | 0.0001448 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 105.3411° |
| argument of perigee: | 72.1503° |
| revolutions per day: | 15.08844918 |
| mean anomaly at epoch: | 287.9647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|