View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52629U 26145.41424657 +.00000000 +00000-0 +21550-4 0 00005
2 52629 53.2128 284.6503 0001142 100.8699 259.2421 15.08833919 08
| Epoch (UTC): | 25 May 2026 09:56:30 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.6503° |
| argument of perigee: | 100.8699° |
| revolutions per day: | 15.08833919 |
| mean anomaly at epoch: | 259.2421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|