View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52127U 26145.52466843 +.00000000 +00000-0 -11103-3 0 00006
2 52127 53.2146 84.1936 0001506 84.3078 275.8086 15.08817748 08
| Epoch (UTC): | 25 May 2026 12:35:31 |
| Eccentricity: | 0.0001506 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1936° |
| argument of perigee: | 84.3078° |
| revolutions per day: | 15.08817748 |
| mean anomaly at epoch: | 275.8086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|