View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52287U 26145.35905063 +.00000000 +00000-0 +42102-3 0 00008
2 52287 53.2128 124.9368 0001348 84.3867 275.7278 15.08809334 01
| Epoch (UTC): | 25 May 2026 08:37:01 |
| Eccentricity: | 0.0001348 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 124.9368° |
| argument of perigee: | 84.3867° |
| revolutions per day: | 15.08809334 |
| mean anomaly at epoch: | 275.7278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|