View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52140U 26145.55409219 +.00000000 +00000-0 +35609-3 0 00004
2 52140 53.2138 84.0591 0001299 88.8065 271.3076 15.08820197 06
| Epoch (UTC): | 25 May 2026 13:17:53 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.0591° |
| argument of perigee: | 88.8065° |
| revolutions per day: | 15.08820197 |
| mean anomaly at epoch: | 271.3076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|