View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 53537U 26144.57386388 +.00000000 +00000-0 +83883-4 0 00005
2 53537 53.2168 93.4315 0001529 76.1080 284.0082 15.08833021 09
| Epoch (UTC): | 24 May 2026 13:46:21 |
| Eccentricity: | 0.0001529 |
| inclination: | 53.2168° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 93.4315° |
| argument of perigee: | 76.1080° |
| revolutions per day: | 15.08833021 |
| mean anomaly at epoch: | 284.0082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|